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 23275.41960264 .00039597 00000-0 64359-2 0 9997
2 00085 38.7539 313.4481 0306120 302.8959 54.2685 14.43790553102770
| Epoch (UTC): | 02 October 2023 10:04:13 |
| Eccentricity: | 0.0306120 |
| inclination: | 38.7539° |
| perigee height: | 528 km |
| apogee height: | 964 km |
| right ascension of ascending node: | 313.4481° |
| argument of perigee: | 302.8959° |
| revolutions per day: | 14.43790553 |
| mean anomaly at epoch: | 54.2685° |
| orbit number at epoch: | 10277 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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