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 56992U 23084BU 25018.82699008 .00338510 00000-0 20408-2 0 9992
2 56992 97.5297 152.0560 0008768 307.3341 52.7125 15.76687271 89460
| Epoch (UTC): | 18 January 2025 19:50:51 |
| Eccentricity: | 0.0008768 |
| inclination: | 97.5297° |
| perigee height: | 334 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 152.0560° |
| argument of perigee: | 307.3341° |
| revolutions per day: | 15.76687271 |
| mean anomaly at epoch: | 52.7125° |
| orbit number at epoch: | 8946 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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