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 28909U 05048B 23088.50259398 .00000033 00000-0 14186-3 0 9996
2 28909 82.4745 341.6502 0006781 271.2129 88.8184 12.55222177791173
| Epoch (UTC): | 29 March 2023 12:03:44 |
| Eccentricity: | 0.0006781 |
| inclination: | 82.4745° |
| perigee height: | 1437 km |
| apogee height: | 1448 km |
| right ascension of ascending node: | 341.6502° |
| argument of perigee: | 271.2129° |
| revolutions per day: | 12.55222177 |
| mean anomaly at epoch: | 88.8184° |
| orbit number at epoch: | 79117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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