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 41502U 00055MA 22221.39004246 .00001241 00000-0 69760-3 0 9998
2 41502 98.7486 280.1331 0011372 194.9273 165.1565 14.12272544331832
| Epoch (UTC): | 09 August 2022 09:21:39 |
| Eccentricity: | 0.0011372 |
| inclination: | 98.7486° |
| perigee height: | 843 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 280.1331° |
| argument of perigee: | 194.9273° |
| revolutions per day: | 14.12272544 |
| mean anomaly at epoch: | 165.1565° |
| orbit number at epoch: | 33183 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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