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 62970U 26145.51558777 +.00000000 +00000-0 +65081-3 0 00003
2 62970 53.1601 235.3415 0001590 104.4227 255.6950 15.30214746 05
| Epoch (UTC): | 25 May 2026 12:22:26 |
| Eccentricity: | 0.0001590 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.3415° |
| argument of perigee: | 104.4227° |
| revolutions per day: | 15.30214746 |
| mean anomaly at epoch: | 255.6950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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