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 23030.57143115 .00007894 00000-0 15020-2 0 9997
2 00085 38.7643 153.5362 0359362 69.7351 294.1648 14.30088217 67562
| Epoch (UTC): | 30 January 2023 13:42:51 |
| Eccentricity: | 0.0359362 |
| inclination: | 38.7643° |
| perigee height: | 534 km |
| apogee height: | 1049 km |
| right ascension of ascending node: | 153.5362° |
| argument of perigee: | 69.7351° |
| revolutions per day: | 14.30088217 |
| mean anomaly at epoch: | 294.1648° |
| orbit number at epoch: | 6756 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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