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 23268.29354802 .00114521 00000-0 18588-1 0 9993
2 00085 38.7575 351.1445 0308121 253.7227 102.9428 14.43165089101746
| Epoch (UTC): | 25 September 2023 07:02:42 |
| Eccentricity: | 0.0308121 |
| inclination: | 38.7575° |
| perigee height: | 528 km |
| apogee height: | 967 km |
| right ascension of ascending node: | 351.1445° |
| argument of perigee: | 253.7227° |
| revolutions per day: | 14.43165089 |
| mean anomaly at epoch: | 102.9428° |
| orbit number at epoch: | 10174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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