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 23150.84426138 .00006495 00000-0 34002-3 0 9990
2 26960 97.7834 181.5403 0045697 330.5580 29.3078 15.15275055181825
| Epoch (UTC): | 30 May 2023 20:15:44 |
| Eccentricity: | 0.0045697 |
| inclination: | 97.7834° |
| perigee height: | 488 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 181.5403° |
| argument of perigee: | 330.5580° |
| revolutions per day: | 15.15275055 |
| mean anomaly at epoch: | 29.3078° |
| orbit number at epoch: | 18182 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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