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 62490U 26145.47576090 +.00000000 +00000-0 +50218-3 0 00009
2 62490 42.9983 215.4410 0001525 277.6993 82.3685 15.27591129 05
| Epoch (UTC): | 25 May 2026 11:25:05 |
| Eccentricity: | 0.0001525 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.4410° |
| argument of perigee: | 277.6993° |
| revolutions per day: | 15.27591129 |
| mean anomaly at epoch: | 82.3685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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