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 27844U 03031E 22274.00634436 .00000315 00000-0 16070-3 0 9991
2 27844 98.6812 280.1112 0010348 150.6617 209.5143 14.22501824998917
| Epoch (UTC): | 01 October 2022 00:09:08 |
| Eccentricity: | 0.0010348 |
| inclination: | 98.6812° |
| perigee height: | 809 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 280.1112° |
| argument of perigee: | 150.6617° |
| revolutions per day: | 14.22501824 |
| mean anomaly at epoch: | 209.5143° |
| orbit number at epoch: | 99891 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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