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 data is extracted from the following two-line orbital elements,
1 42834U 17042K 25345.00500457 .00009716 00000-0 65815-3 0 9996
2 42834 97.3999 148.3099 0009088 356.7711 3.3457 15.06644281458622
| Epoch (UTC): | 11 December 2025 00:07:12 |
| Eccentricity: | 0.0009088 |
| inclination: | 97.3999° |
| perigee height: | 540 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 148.3099° |
| argument of perigee: | 356.7711° |
| revolutions per day: | 15.06644281 |
| mean anomaly at epoch: | 3.3457° |
| orbit number at epoch: | 45862 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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