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 57940U 26145.40176000 +.00000000 +00000-0 +70803-4 0 00006
2 57940 53.1618 28.1476 0001394 91.7461 268.3700 15.30184845 09
| Epoch (UTC): | 25 May 2026 09:38:32 |
| Eccentricity: | 0.0001394 |
| inclination: | 53.1618° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 28.1476° |
| argument of perigee: | 91.7461° |
| revolutions per day: | 15.30184845 |
| mean anomaly at epoch: | 268.3700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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