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 62801U 26145.61220811 +.00000000 +00000-0 +14005-3 0 00002
2 62801 88.9724 86.0752 0013597 231.3627 128.6308 13.51013668 06
| Epoch (UTC): | 25 May 2026 14:41:34 |
| Eccentricity: | 0.0013597 |
| inclination: | 88.9724° |
| perigee height: | 1058 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 86.0752° |
| argument of perigee: | 231.3627° |
| revolutions per day: | 13.51013668 |
| mean anomaly at epoch: | 128.6308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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