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 23084.18459889 .00000612 00000-0 26442-3 0 9998
2 26931 67.0515 53.7154 0006969 282.8517 77.1805 14.30864670121725
| Epoch (UTC): | 25 March 2023 04:25:49 |
| Eccentricity: | 0.0006969 |
| inclination: | 67.0515° |
| perigee height: | 784 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 53.7154° |
| argument of perigee: | 282.8517° |
| revolutions per day: | 14.30864670 |
| mean anomaly at epoch: | 77.1805° |
| orbit number at epoch: | 12172 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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