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 62796U 26145.58752962 +.00000000 +00000-0 +11656-3 0 00007
2 62796 88.9736 86.0405 0013100 220.0267 139.9920 13.51013509 01
| Epoch (UTC): | 25 May 2026 14:06:02 |
| Eccentricity: | 0.0013100 |
| inclination: | 88.9736° |
| perigee height: | 1059 km |
| apogee height: | 1078 km |
| right ascension of ascending node: | 86.0405° |
| argument of perigee: | 220.0267° |
| revolutions per day: | 13.51013509 |
| mean anomaly at epoch: | 139.9920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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