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 22825U 26108.91383786 +.00000000 +00000-0 +43144-4 0 00004
2 22825 98.6914 176.3390 0007223 274.6548 85.3810 14.30925856 05
| Epoch (UTC): | 18 April 2026 21:55:55 |
| Eccentricity: | 0.0007223 |
| inclination: | 98.6914° |
| perigee height: | 783 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 176.3390° |
| argument of perigee: | 274.6548° |
| revolutions per day: | 14.30925856 |
| mean anomaly at epoch: | 85.3810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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