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 27869U 03037B 23088.49024702 .00000050 00000-0 27697-3 0 9993
2 27869 82.4747 343.9107 0023131 103.2382 257.1282 12.45469583891554
| Epoch (UTC): | 29 March 2023 11:45:57 |
| Eccentricity: | 0.0023131 |
| inclination: | 82.4747° |
| perigee height: | 1465 km |
| apogee height: | 1501 km |
| right ascension of ascending node: | 343.9107° |
| argument of perigee: | 103.2382° |
| revolutions per day: | 12.45469583 |
| mean anomaly at epoch: | 257.1282° |
| orbit number at epoch: | 89155 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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