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 62793U 26145.59570980 +.00000000 +00000-0 +83617-4 0 00000
2 62793 88.9734 86.0651 0014000 231.5398 128.4497 13.51004658 08
| Epoch (UTC): | 25 May 2026 14:17:49 |
| Eccentricity: | 0.0014000 |
| inclination: | 88.9734° |
| perigee height: | 1058 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 86.0651° |
| argument of perigee: | 231.5398° |
| revolutions per day: | 13.51004658 |
| mean anomaly at epoch: | 128.4497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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