View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 61971U 26145.36371955 +.00000000 +00000-0 +55281-3 0 00008
2 61971 43.0014 107.0310 0001471 268.4321 91.6362 15.27593492 03
| Epoch (UTC): | 25 May 2026 08:43:45 |
| Eccentricity: | 0.0001471 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.0310° |
| argument of perigee: | 268.4321° |
| revolutions per day: | 15.27593492 |
| mean anomaly at epoch: | 91.6362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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