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 is defined by the following mean orbital elements,
1 26621U 26159.82298433 +.00000000 +00000-0 -62891-3 0 00002
2 26621 95.4101 87.4837 0708965 273.5736 78.4631 13.04826437 01
| Epoch (UTC): | 08 June 2026 19:45:05 |
| Eccentricity: | 0.0708965 |
| inclination: | 95.4101° |
| perigee height: | 703 km |
| apogee height: | 1784 km |
| right ascension of ascending node: | 87.4837° |
| argument of perigee: | 273.5736° |
| revolutions per day: | 13.04826437 |
| mean anomaly at epoch: | 78.4631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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