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 67250U 26145.11224814 +.00000000 +00000-0 +11747-3 0 00007
2 67250 97.6178 216.6993 0153366 54.1085 307.4258 14.88188746 07
| Epoch (UTC): | 25 May 2026 02:41:38 |
| Eccentricity: | 0.0153366 |
| inclination: | 97.6178° |
| perigee height: | 497 km |
| apogee height: | 711 km |
| right ascension of ascending node: | 216.6993° |
| argument of perigee: | 54.1085° |
| revolutions per day: | 14.88188746 |
| mean anomaly at epoch: | 307.4258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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