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 26294U 26088.14528072 +.00000000 +00000-0 +53791-3 0 00007
2 26294 98.4716 157.6085 0077887 72.1309 348.6774 14.55130073 09
| Epoch (UTC): | 29 March 2026 03:29:12 |
| Eccentricity: | 0.0077887 |
| inclination: | 98.4716° |
| perigee height: | 654 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 157.6085° |
| argument of perigee: | 72.1309° |
| revolutions per day: | 14.55130073 |
| mean anomaly at epoch: | 348.6774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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