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 21891U 92009B 23270.33943707 .00004074 00000-0 40135-3 0 9992
2 21891 19.9959 136.0567 0044279 333.0674 26.7451 14.86031258686334
| Epoch (UTC): | 27 September 2023 08:08:47 |
| Eccentricity: | 0.0044279 |
| inclination: | 19.9959° |
| perigee height: | 579 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 136.0567° |
| argument of perigee: | 333.0674° |
| revolutions per day: | 14.86031258 |
| mean anomaly at epoch: | 26.7451° |
| orbit number at epoch: | 68633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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