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 26694U 01005A 25093.57857635 0.00000000 00000-0 00000-0 0 01
2 26694 11.5272 33.4527 0008502 146.4402 213.6258 0.98739767 00
| Epoch (UTC): | 03 April 2025 13:53:08 |
| Eccentricity: | 0.0008502 |
| inclination: | 11.5272° |
| perigee height: | 36185 km |
| apogee height: | 36257 km |
| right ascension of ascending node: | 33.4527° |
| argument of perigee: | 146.4402° |
| revolutions per day: | 0.98739767 |
| mean anomaly at epoch: | 213.6258° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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