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 23097U 94026A 25165.93580718 0.00000000 00000-0 00000-0 0 05
2 23097 62.5802 180.5554 6629601 263.8032 96.1975 2.00604814 00
| Epoch (UTC): | 14 June 2025 22:27:33 |
| Eccentricity: | 0.6629601 |
| inclination: | 62.5802° |
| perigee height: | 2572 km |
| apogee height: | 37784 km |
| right ascension of ascending node: | 180.5554° |
| argument of perigee: | 263.8032° |
| revolutions per day: | 2.00604814 |
| mean anomaly at epoch: | 96.1975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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