BLUE RING PATHFINDER, 62720
Orbit data source: Space-Track
BLUE RING PATHFINDER, 62720 is a payload satellite owned by Blue Origin (US) in HEO that was launched on Thu, 16 Jan 2025 UTC via an NEW GLENN 7X2 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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62720 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Blue Origin
Mission
Non-operational Commercial Technology
Bus & Motor
BLUE RING, Unknown motor
Mass
~33,980 kg wet, ~3,980 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + Ann Cyl + Box, 14.5 m
Radar Cross Section
272.300 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 BLUE RING PATHFINDER
1 62720U 25011A 26096.85559075 .00000002 00000-0 00000-0 0 9995
2 62720 29.7882 191.3884 4893493 234.0781 70.1436 3.84310570 17138Epoch: 2026-04-06T20:32Z
TLE epoch observation values (Epoch: 2026-04-06T20:32:03.040Z)
Latitude
0.00004°
Longitude
48.25577°
Altitude
12,003.016 km
Speed
4.497 km/s
True Right ascension
12h 45m 38s
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
09:47:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,267.002 km
Perigee altitude
2,414.769 km
Semi-major axis
17,219.023 km
Eccentricity
0.48935
Inclination
29.7882°
RAAN
191.3884°
Arg. of periapsis
234.0781°
True anomaly
125.97678°
Mean anomaly
70.1436°
Eccentric anomaly
97.9142°
Mean motion
0.96057 °/min
Orbital period
374.78 mins
BSTAR
0
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Other satellites on launch #11 in the year 2025 (2025-01-16 UTC)
No other RSOs were in this launch
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.BLUE RING PATHFINDER 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. |
|---|---|---|---|---|---|---|---|
| 187 mins | 2026-04-08 03:42:18.582Z | 125.374° SE | 2026-04-08 05:11:18.582Z | 91.39° ESE | 19.391° | 2026-04-08 06:49:18.582Z | 72.164° E |
| 270 mins | 2026-04-08 10:02:18.582Z | 242.044° WSW | 2026-04-08 13:35:18.582Z | 194.949° SSW | 43.877° | 2026-04-08 14:32:18.582Z | 116.614° SE |
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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