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 62258U 26143.73594177 +.00000000 +00000-0 +57230-2 0 00004
2 62258 59.6991 99.5464 8005506 204.8721 70.7768 1.22073745 05
| Epoch (UTC): | 23 May 2026 17:39:45 |
| Eccentricity: | 0.8005506 |
| inclination: | 59.6991° |
| perigee height: | 998 km |
| apogee height: | 60209 km |
| right ascension of ascending node: | 99.5464° |
| argument of perigee: | 204.8721° |
| revolutions per day: | 1.22073745 |
| mean anomaly at epoch: | 70.7768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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