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 00005U 58002B 22331.79781111 .00000110 00000-0 16412-3 0 9995
2 00005 34.2490 356.0074 1845757 52.8277 322.7037 10.85037330302281
| Epoch (UTC): | 27 November 2022 19:08:50 |
| Eccentricity: | 0.1845757 |
| inclination: | 34.2490° |
| perigee height: | 650 km |
| apogee height: | 3831 km |
| right ascension of ascending node: | 356.0074° |
| argument of perigee: | 52.8277° |
| revolutions per day: | 10.85037330 |
| mean anomaly at epoch: | 322.7037° |
| orbit number at epoch: | 30228 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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