BALKAN-1, 62611
Orbit data source: Space-Track
BALKAN-1, 62611 is a payload satellite owned by Endurosat (BG) 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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62611 intel report (Beta)
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Identifier
Orbit
Country
BG / BGRRelated business
Manufacturer
Endurosat
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
32 kg wet, 32 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.124 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 BALKAN-1
1 62611U 25009C 26306.78312036 .00005274 00000-0 20412-3 0 9999
2 62611 97.3820 24.3518 0006124 190.9235 169.1872 15.26607974 99898Epoch: 2026-11-02T18:47Z
TLE epoch observation values (Epoch: 2026-11-02T18:47:41.599Z)
Latitude
0.00002°
Longitude
60.37328°
Altitude
493.191 km
Speed
7.616 km/s
True Right ascension
01h 37m 24s
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
08:42:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.119 km
Perigee altitude
478.716 km
Semi-major axis
6,861.054 km
Eccentricity
0.00061
Inclination
97.382°
RAAN
24.3518°
Arg. of periapsis
190.9235°
True anomaly
169.20036°
Mean anomaly
169.1872°
Eccentric anomaly
169.19378°
Mean motion
3.81906 °/min
Orbital period
94.26 mins
BSTAR
0.00020412
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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.BALKAN-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 | 2026-11-03 17:24:18.227Z | 57.445° ENE | 2026-11-03 17:26:18.227Z | 99.455° ESE | 19.847° | 2026-11-03 17:28:18.227Z | 137.801° SSE |
| 4 mins | 2026-11-03 18:58:18.227Z | 318.584° NNW | 2026-11-03 18:59:18.227Z | 294.979° NW | 22.325° | 2026-11-03 19:02:18.227Z | 237.568° WSW |
| 5 mins | 2026-11-04 05:32:18.227Z | 180.275° SSW | 2026-11-04 05:34:18.227Z | 224.317° SW | 61.202° | 2026-11-04 05:37:18.227Z | 339.447° 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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