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 23156.65526002 .00006273 00000-0 32799-3 0 9991
2 26960 97.7821 187.4926 0045211 310.0270 49.6998 15.15356249182706
| Epoch (UTC): | 05 June 2023 15:43:34 |
| Eccentricity: | 0.0045211 |
| inclination: | 97.7821° |
| perigee height: | 489 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 187.4926° |
| argument of perigee: | 310.0270° |
| revolutions per day: | 15.15356249 |
| mean anomaly at epoch: | 49.6998° |
| orbit number at epoch: | 18270 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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