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 35895U 93036AUJ 23325.98772296 .00003040 00000-0 18524-2 0 9995
2 35895 74.0502 205.5213 0219505 118.7640 243.5735 13.95222079495790
| Epoch (UTC): | 21 November 2023 23:42:19 |
| Eccentricity: | 0.0219505 |
| inclination: | 74.0502° |
| perigee height: | 750 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 205.5213° |
| argument of perigee: | 118.7640° |
| revolutions per day: | 13.95222079 |
| mean anomaly at epoch: | 243.5735° |
| orbit number at epoch: | 49579 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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