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 00085U 61004C 23035.59924541 .00016828 00000-0 31719-2 0 9994
2 00085 38.7651 127.4976 0358508 103.7392 260.3523 14.30243717 68282
| Epoch (UTC): | 04 February 2023 14:22:54 |
| Eccentricity: | 0.0358508 |
| inclination: | 38.7651° |
| perigee height: | 534 km |
| apogee height: | 1048 km |
| right ascension of ascending node: | 127.4976° |
| argument of perigee: | 103.7392° |
| revolutions per day: | 14.30243717 |
| mean anomaly at epoch: | 260.3523° |
| orbit number at epoch: | 6828 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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