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 60907U 26145.61445676 +.00000000 +00000-0 +12588-4 0 00000
2 60907 53.1597 112.2477 0001167 72.5052 287.6093 15.69708723 07
| Epoch (UTC): | 25 May 2026 14:44:49 |
| Eccentricity: | 0.0001167 |
| inclination: | 53.1597° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 112.2477° |
| argument of perigee: | 72.5052° |
| revolutions per day: | 15.69708723 |
| mean anomaly at epoch: | 287.6093° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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