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 24277U 96046A 22147.86631066 .00000162 00000-0 81774-4 0 9999
2 24277 98.9337 150.2084 0002335 98.3207 261.8238 14.29538350343960
| Epoch (UTC): | 27 May 2022 20:47:29 |
| Eccentricity: | 0.0002335 |
| inclination: | 98.9337° |
| perigee height: | 791 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 150.2084° |
| argument of perigee: | 98.3207° |
| revolutions per day: | 14.29538350 |
| mean anomaly at epoch: | 261.8238° |
| orbit number at epoch: | 34396 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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