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 4659U 70025AT 23335.62557637 .00002884 00000-0 24200-2 0 9997
2 4659 100.1255 1.6866 0011789 186.0814 174.0199 13.89002090679983
| Epoch (UTC): | 01 December 2023 15:00:49 |
| Eccentricity: | 0.0011789 |
| inclination: | 100.1255° |
| perigee height: | 923 km |
| apogee height: | 941 km |
| right ascension of ascending node: | 1.6866° |
| argument of perigee: | 186.0814° |
| revolutions per day: | 13.89002090 |
| mean anomaly at epoch: | 174.0199° |
| orbit number at epoch: | 67998 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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