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 26960U 01049D 22139.52543968 .00007594 00000-0 45340-3 0 9990
2 26960 97.8156 157.0038 0052439 174.2788 185.9051 15.10246148124957
| Epoch (UTC): | 19 May 2022 12:36:37 |
| Eccentricity: | 0.0052439 |
| inclination: | 97.8156° |
| perigee height: | 499 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 157.0038° |
| argument of perigee: | 174.2788° |
| revolutions per day: | 15.10246148 |
| mean anomaly at epoch: | 185.9051° |
| orbit number at epoch: | 12495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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