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 26073.18223763 +.00000000 +00000-0 +61916-4 0 00009
2 22825 98.6972 140.5955 0008738 26.6550 333.5080 14.30914705 07
| Epoch (UTC): | 14 March 2026 04:22:25 |
| Eccentricity: | 0.0008738 |
| inclination: | 98.6972° |
| perigee height: | 782 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 140.5955° |
| argument of perigee: | 26.6550° |
| revolutions per day: | 14.30914705 |
| mean anomaly at epoch: | 333.5080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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