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 07615U 26099.83240873 +.00000000 +00000-0 -10573-3 0 00003
2 07615 99.0339 56.1694 0009194 134.1866 226.0054 13.96970149 05
| Epoch (UTC): | 09 April 2026 19:58:40 |
| Eccentricity: | 0.0009194 |
| inclination: | 99.0339° |
| perigee height: | 898 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 56.1694° |
| argument of perigee: | 134.1866° |
| revolutions per day: | 13.96970149 |
| mean anomaly at epoch: | 226.0054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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