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 25544U 98067A 23336.48733383 .00030290 00000-0 53530-3 0 9999
2 25544 51.6412 214.9466 0001301 3.2675 56.9965 15.50073145427892
| Epoch (UTC): | 02 December 2023 11:41:45 |
| Eccentricity: | 0.0001301 |
| inclination: | 51.6412° |
| perigee height: | 415 km |
| apogee height: | 417 km |
| right ascension of ascending node: | 214.9466° |
| argument of perigee: | 3.2675° |
| revolutions per day: | 15.50073145 |
| mean anomaly at epoch: | 56.9965° |
| orbit number at epoch: | 42789 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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