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 23153.08945634 .00007818 00000-0 40813-3 0 9993
2 26960 97.7831 183.8400 0045451 322.6431 37.1642 15.15311077182166
| Epoch (UTC): | 02 June 2023 02:08:49 |
| Eccentricity: | 0.0045451 |
| inclination: | 97.7831° |
| perigee height: | 488 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 183.8400° |
| argument of perigee: | 322.6431° |
| revolutions per day: | 15.15311077 |
| mean anomaly at epoch: | 37.1642° |
| orbit number at epoch: | 18216 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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