SIGI, 62632
Orbit data source: Space-Track
SIGI, 62632 is a German payload satellite in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62632 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
REFLEX
Mission
Operational Commercial Communications
Bus & Motor
OMNIFLEX, Unknown motor
Mass
109 kg wet, 109 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.5 m
Radar Cross Section
1.176 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 SIGI
1 62632U 25009Z 25258.53166263 .00005316 00000-0 24474-3 0 9998
2 62632 97.4249 337.3817 0003641 170.8449 189.2853 15.20725101 37005Epoch: 2025-09-15T12:45Z
TLE epoch observation values (Epoch: 2025-09-15T12:45:35.651Z)
Latitude
-0.00006°
Longitude
151.24819°
Altitude
509.216 km
Speed
7.608 km/s
True Right ascension
22h 29m 31s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
18:07:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.122 km
Perigee altitude
498.113 km
Semi-major axis
6,878.755 km
Eccentricity
0.00036
Inclination
97.4249°
RAAN
337.3817°
Arg. of periapsis
170.8449°
True anomaly
189.27857°
Mean anomaly
189.2853°
Eccentric anomaly
189.28194°
Mean motion
3.80433 °/min
Orbital period
94.63 mins
BSTAR
0.00024474
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SIGI Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-16 04:41:17.823Z | 126.501° SE | 2025-09-16 04:44:17.823Z | 70.204° E | 23.139° | 2025-09-16 04:47:17.823Z | 14.658° NNE |
| 5 mins | 2025-09-16 17:46:17.823Z | 45.055° ENE | 2025-09-16 17:48:17.823Z | 105.674° ESE | 30.632° | 2025-09-16 17:51:17.823Z | 165.362° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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