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 23158.50852449 .00010334 00000-0 18754-2 0 9998
2 00085 38.7595 207.7998 0332475 219.4850 138.1236 14.35900162 85926
| Epoch (UTC): | 07 June 2023 12:12:16 |
| Eccentricity: | 0.0332475 |
| inclination: | 38.7595° |
| perigee height: | 534 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 207.7998° |
| argument of perigee: | 219.4850° |
| revolutions per day: | 14.35900162 |
| mean anomaly at epoch: | 138.1236° |
| orbit number at epoch: | 8592 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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