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 29049U 06011C 23088.85137570 .00000902 00000-0 36795-3 0 9993
2 29049 72.0186 284.0875 0033180 88.1440 272.3497 14.29332990884628
| Epoch (UTC): | 29 March 2023 20:25:58 |
| Eccentricity: | 0.0033180 |
| inclination: | 72.0186° |
| perigee height: | 770 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 284.0875° |
| argument of perigee: | 88.1440° |
| revolutions per day: | 14.29332990 |
| mean anomaly at epoch: | 272.3497° |
| orbit number at epoch: | 88462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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