ELEVATION-1, 62677
Orbit data source: Space-Track
ELEVATION-1, 62677 is a UK 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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62677 intel report (Beta)
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Identifier
Orbit
Country
UKRelated business
Manufacturer
XDLINX
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ELEVATION-1
1 62677U 25009BW 26079.47496757 .00016909 00000-0 46581-3 0 9999
2 62677 97.3886 163.9056 0003123 264.7455 95.3433 15.37206448123174Epoch: 2026-03-20T11:23Z
TLE epoch observation values (Epoch: 2026-03-20T11:23:57.198Z)
Latitude
-0.00001°
Longitude
174.90777°
Altitude
457.688 km
Speed
7.638 km/s
True Right ascension
10h 55m 37s
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
16:02:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
453.45 km
Perigee altitude
449.184 km
Semi-major axis
6,829.454 km
Eccentricity
0.00031
Inclination
97.3886°
RAAN
163.9056°
Arg. of periapsis
264.7455°
True anomaly
95.37893°
Mean anomaly
95.3433°
Eccentric anomaly
95.36112°
Mean motion
3.8456 °/min
Orbital period
93.61 mins
BSTAR
0.00046581
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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.ELEVATION-1 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-03-21 17:39:55.699Z | 58.188° ENE | 2026-03-21 17:41:55.699Z | 101.794° ESE | 17.955° | 2026-03-21 17:43:55.699Z | 139.833° SSE |
| 4 mins | 2026-03-21 19:12:55.699Z | 323.812° NNW | 2026-03-21 19:13:55.699Z | 301.953° NW | 19.042° | 2026-03-21 19:16:55.699Z | 240.453° WSW |
| 5 mins | 2026-03-22 05:42:55.699Z | 175.242° S | 2026-03-22 05:44:55.699Z | 213.254° SW | 42.73° | 2026-03-22 05:47:55.699Z | 342.966° N |
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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