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 23609U 95034A 25165.75720220 0.00000000 00000-0 00000-0 0 08
2 23609 63.2462 151.4213 6734122 272.0521 18.1212 2.00591770 02
| Epoch (UTC): | 14 June 2025 18:10:22 |
| Eccentricity: | 0.6734122 |
| inclination: | 63.2462° |
| perigee height: | 2295 km |
| apogee height: | 38064 km |
| right ascension of ascending node: | 151.4213° |
| argument of perigee: | 272.0521° |
| revolutions per day: | 2.00591770 |
| mean anomaly at epoch: | 18.1212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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