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 29249U 06027A 23059.80933803 0.00000000 00000-0 00000-0 0 07
2 29249 63.4721 34.2318 7192071 272.8806 87.1194 2.00630027 02
| Epoch (UTC): | 28 February 2023 19:25:26 |
| Eccentricity: | 0.7192071 |
| inclination: | 63.4721° |
| perigee height: | 1078 km |
| apogee height: | 39274 km |
| right ascension of ascending node: | 34.2318° |
| argument of perigee: | 272.8806° |
| revolutions per day: | 2.00630027 |
| mean anomaly at epoch: | 87.1194° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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