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 39953U 81053NP 25226.51591066 .00000122 00000-0 13908-3 0 9995
2 39953 82.9728 322.8720 0179235 67.2313 306.8259 13.55031655 12134
| Epoch (UTC): | 14 August 2025 12:22:54 |
| Eccentricity: | 0.0179235 |
| inclination: | 82.9728° |
| perigee height: | 920 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 322.8720° |
| argument of perigee: | 67.2313° |
| revolutions per day: | 13.55031655 |
| mean anomaly at epoch: | 306.8259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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