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 22739U 26088.11394141 +.00000000 +00000-0 +84870-4 0 00005
2 22739 98.6963 35.3224 0009587 5.1611 354.9659 14.13642657 08
| Epoch (UTC): | 29 March 2026 02:44:04 |
| Eccentricity: | 0.0009587 |
| inclination: | 98.6963° |
| perigee height: | 840 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 35.3224° |
| argument of perigee: | 5.1611° |
| revolutions per day: | 14.13642657 |
| mean anomaly at epoch: | 354.9659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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