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 26722U 26075.46193613 +.00000000 +00000-0 +66735-2 0 00004
2 26722 2.4490 343.2536 7072397 87.4552 344.3966 2.22953140 05
| Epoch (UTC): | 16 March 2026 11:05:11 |
| Eccentricity: | 0.7072397 |
| inclination: | 2.4490° |
| perigee height: | 868 km |
| apogee height: | 35878 km |
| right ascension of ascending node: | 343.2536° |
| argument of perigee: | 87.4552° |
| revolutions per day: | 2.22953140 |
| mean anomaly at epoch: | 344.3966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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