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 51994C 22025AQ 24358.52756944 -.00001184 00000+0 -74306-4 0 3581
2 51994 53.2148 199.5725 0002243 86.3095 30.5029 15.08811922 10
| Epoch (UTC): | 23 December 2024 12:39:42 |
| Eccentricity: | 0.0002243 |
| inclination: | 53.2148° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 199.5725° |
| argument of perigee: | 86.3095° |
| revolutions per day: | 15.08811922 |
| mean anomaly at epoch: | 30.5029° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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