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 25194.47520423 .00033495 00000-0 55761-3 0 9996
2 26960 97.6759 265.5244 0022636 129.4625 230.8634 15.51669522300139
| Epoch (UTC): | 13 July 2025 11:24:17 |
| Eccentricity: | 0.0022636 |
| inclination: | 97.6759° |
| perigee height: | 396 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 265.5244° |
| argument of perigee: | 129.4625° |
| revolutions per day: | 15.51669522 |
| mean anomaly at epoch: | 230.8634° |
| orbit number at epoch: | 30013 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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