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 62489U 26145.55270771 +.00000000 +00000-0 +39996-3 0 00003
2 62489 42.9988 215.1551 0001463 273.9507 86.1178 15.27587712 04
| Epoch (UTC): | 25 May 2026 13:15:53 |
| Eccentricity: | 0.0001463 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.1551° |
| argument of perigee: | 273.9507° |
| revolutions per day: | 15.27587712 |
| mean anomaly at epoch: | 86.1178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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