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 26931U 01043C 23081.66824412 .00000419 00000-0 19083-3 0 9994
2 26931 67.0510 60.2124 0006934 283.1154 76.9174 14.30860760121365
| Epoch (UTC): | 22 March 2023 16:02:16 |
| Eccentricity: | 0.0006934 |
| inclination: | 67.0510° |
| perigee height: | 784 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 60.2124° |
| argument of perigee: | 283.1154° |
| revolutions per day: | 14.30860760 |
| mean anomaly at epoch: | 76.9174° |
| orbit number at epoch: | 12136 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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