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 57870U 26145.49668968 +.00000000 +00000-0 +33859-4 0 00006
2 57870 43.0024 211.4754 0001365 279.6490 80.4207 15.27576344 03
| Epoch (UTC): | 25 May 2026 11:55:13 |
| Eccentricity: | 0.0001365 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.4754° |
| argument of perigee: | 279.6490° |
| revolutions per day: | 15.27576344 |
| mean anomaly at epoch: | 80.4207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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