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 00045U 60007A 25142.58035703 .00000416 00000-0 12976-3 0 9996
2 00045 66.6939 313.0428 0242365 84.1027 278.7642 14.35536726323977
| Epoch (UTC): | 22 May 2025 13:55:42 |
| Eccentricity: | 0.0242365 |
| inclination: | 66.6939° |
| perigee height: | 600 km |
| apogee height: | 946 km |
| right ascension of ascending node: | 313.0428° |
| argument of perigee: | 84.1027° |
| revolutions per day: | 14.35536726 |
| mean anomaly at epoch: | 278.7642° |
| orbit number at epoch: | 32397 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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