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 22827U 26088.14680649 +.00000000 +00000-0 +86456-4 0 00009
2 22827 98.6469 156.8046 0007726 261.5320 162.2813 14.32514135 08
| Epoch (UTC): | 29 March 2026 03:31:24 |
| Eccentricity: | 0.0007726 |
| inclination: | 98.6469° |
| perigee height: | 778 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 156.8046° |
| argument of perigee: | 261.5320° |
| revolutions per day: | 14.32514135 |
| mean anomaly at epoch: | 162.2813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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