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 62071U 26145.51647375 +.00000000 +00000-0 +59998-3 0 00008
2 62071 53.1595 197.0635 0001407 59.9726 300.1417 15.34400260 08
| Epoch (UTC): | 25 May 2026 12:23:43 |
| Eccentricity: | 0.0001407 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 197.0635° |
| argument of perigee: | 59.9726° |
| revolutions per day: | 15.34400260 |
| mean anomaly at epoch: | 300.1417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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