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 85U 61004C 23334.12467634 .00041590 00000-0 63368-2 0 9999
2 85 38.7516 1.6852 0290722 351.1533 8.4170 14.48561618111243
| Epoch (UTC): | 30 November 2023 02:59:32 |
| Eccentricity: | 0.0290722 |
| inclination: | 38.7516° |
| perigee height: | 523 km |
| apogee height: | 937 km |
| right ascension of ascending node: | 1.6852° |
| argument of perigee: | 351.1533° |
| revolutions per day: | 14.48561618 |
| mean anomaly at epoch: | 8.4170° |
| orbit number at epoch: | 11124 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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