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 35499U 09036B 23088.45518609 .00000046 00000-0 26148-3 0 9991
2 35499 82.4849 91.8210 0016260 179.0590 181.0523 12.42949865622701
| Epoch (UTC): | 29 March 2023 10:55:28 |
| Eccentricity: | 0.0016260 |
| inclination: | 82.4849° |
| perigee height: | 1481 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 91.8210° |
| argument of perigee: | 179.0590° |
| revolutions per day: | 12.42949865 |
| mean anomaly at epoch: | 181.0523° |
| orbit number at epoch: | 62270 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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