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 22027.01984828 .00003798 00000-0 81276-3 0 9991
2 00085 38.7644 253.4702 0373989 109.2394 254.9199 14.23710266 14890
| Epoch (UTC): | 27 January 2022 00:28:34 |
| Eccentricity: | 0.0373989 |
| inclination: | 38.7644° |
| perigee height: | 544 km |
| apogee height: | 1082 km |
| right ascension of ascending node: | 253.4702° |
| argument of perigee: | 109.2394° |
| revolutions per day: | 14.23710266 |
| mean anomaly at epoch: | 254.9199° |
| orbit number at epoch: | 1489 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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