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 00012U 59001B 23342.24986375 .00000319 00000-0 16544-3 0 9992
2 00012 32.9098 228.2795 1660348 271.8337 69.3687 11.45891772425409
| Epoch (UTC): | 08 December 2023 05:59:48 |
| Eccentricity: | 0.1660348 |
| inclination: | 32.9098° |
| perigee height: | 553 km |
| apogee height: | 3312 km |
| right ascension of ascending node: | 228.2795° |
| argument of perigee: | 271.8337° |
| revolutions per day: | 11.45891772 |
| mean anomaly at epoch: | 69.3687° |
| orbit number at epoch: | 42540 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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