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, 0.7 m
Radar Cross Section
0.124 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 BALKAN-1
1 62611U 25009C 26124.76534060 .00007657 00000-0 31440-3 0 9998
2 62611 97.3923 204.5622 0008468 121.9605 238.2457 15.24457251 72143Epoch: 2026-05-04T18:22Z
TLE epoch observation values (Epoch: 2026-05-04T18:22:05.427Z)
Latitude
-0.00004°
Longitude
66.38975°
Altitude
498.579 km
Speed
7.614 km/s
True Right ascension
13h 38m 14s
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
18:33:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.19 km
Perigee altitude
483.56 km
Semi-major axis
6,867.512 km
Eccentricity
0.00085
Inclination
97.3923°
RAAN
204.5622°
Arg. of periapsis
121.9605°
True anomaly
238.16323°
Mean anomaly
238.2457°
Eccentric anomaly
238.20446°
Mean motion
3.81368 °/min
Orbital period
94.4 mins
BSTAR
0.0003144
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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 | 2026-05-05 18:34:47.872Z | 337.442° NNW | 2026-05-05 18:35:47.872Z | 306.297° NW | 32.67° | 2026-05-05 18:38:47.872Z | 219.963° SW |
| 5 mins | 2026-05-06 05:09:47.872Z | 152.873° SSE | 2026-05-06 05:11:47.872Z | 113.067° SE | 39.997° | 2026-05-06 05:14:47.872Z | 357.916° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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