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 62707U 26145.14248044 +.00000000 +00000-0 +24141-3 0 00005
2 62707 97.7052 224.6356 0001647 153.7558 206.3746 14.95852249 01
| Epoch (UTC): | 25 May 2026 03:25:10 |
| Eccentricity: | 0.0001647 |
| inclination: | 97.7052° |
| perigee height: | 579 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 224.6356° |
| argument of perigee: | 153.7558° |
| revolutions per day: | 14.95852249 |
| mean anomaly at epoch: | 206.3746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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