UAPSat-1
UAPSat-1 |
| Mission type |
Technology |
|---|
| Operator |
UAP |
|---|
|
| Spacecraft properties |
|---|
| Spacecraft type |
1U CubeSat |
|---|
| Launch mass |
1 kilogram (2.2 lb) |
|---|
|
| Start of mission |
|---|
| Launch date |
January 9, 2014, 18:07:05 (2014-01-09UTC18:07:05Z) UTC[1] |
|---|
| Rocket |
Antares 120 |
|---|
| Launch site |
MARS LP-0B |
|---|
| Contractor |
Orbital Sciences |
|---|
|
| End of mission |
|---|
| Decay date |
22 May 2014 (2014-05-23) |
|---|
|
| Orbital parameters |
|---|
| Reference system |
Geocentric |
|---|
| Regime |
Low Earth |
|---|
UAPSat-1 was a satellite situated in earth orbit created and operated by students and staff at Universidad Alas Peruanas. It was launched on an Orbital Sciences Corporation Antares rocket alongside Cygnus CRS Orb-1.[2] Orbital decay occurred on July 1, 2014.
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| | November | Sasuke · Hodoyoshi 1 · Kinshachi 1 · Tsukushi · Tsubame | Yaogan 23 | Yaogan 24 | Kuaizhou 2 | Soyuz TMA-15M | Kosmos 2501 |
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| Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets). |
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