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 43137U 18004AC 22141.65875635 .00017638 00000-0 62958-3 0 9994
2 43137 97.3684 217.0646 0009334 98.8536 261.3761 15.28885334242259
| Epoch (UTC): | 21 May 2022 15:48:36 |
| Eccentricity: | 0.0009334 |
| inclination: | 97.3684° |
| perigee height: | 473 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 217.0646° |
| argument of perigee: | 98.8536° |
| revolutions per day: | 15.28885334 |
| mean anomaly at epoch: | 261.3761° |
| orbit number at epoch: | 24225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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