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 22828U 26106.66816367 +.00000000 +00000-0 +47204-4 0 00004
2 22828 98.6892 173.9644 0009059 222.1701 137.8786 14.31775941 00
| Epoch (UTC): | 16 April 2026 16:02:09 |
| Eccentricity: | 0.0009059 |
| inclination: | 98.6892° |
| perigee height: | 779 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 173.9644° |
| argument of perigee: | 222.1701° |
| revolutions per day: | 14.31775941 |
| mean anomaly at epoch: | 137.8786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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