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 29U 60002B 23032.99931869 .00000542 00000-0 11021-3 0 9992
2 29 48.3795 98.9989 0023686 17.3186 342.8530 14.74964922360262
| Epoch (UTC): | 01 February 2023 23:59:01 |
| Eccentricity: | 0.0023686 |
| inclination: | 48.3795° |
| perigee height: | 628 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 98.9989° |
| argument of perigee: | 17.3186° |
| revolutions per day: | 14.74964922 |
| mean anomaly at epoch: | 342.8530° |
| orbit number at epoch: | 36026 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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