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 35498U 09036A 23088.52293263 .00000022 00000-0 92065-4 0 9990
2 35498 82.4842 101.8481 0005939 239.6732 120.3760 12.40835243621897
| Epoch (UTC): | 29 March 2023 12:33:01 |
| Eccentricity: | 0.0005939 |
| inclination: | 82.4842° |
| perigee height: | 1498 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 101.8481° |
| argument of perigee: | 239.6732° |
| revolutions per day: | 12.40835243 |
| mean anomaly at epoch: | 120.3760° |
| orbit number at epoch: | 62189 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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