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 25984U 26088.20670109 +.00000000 +00000-0 +51110-3 0 00001
2 25984 45.0382 179.2319 0004204 268.9357 91.1010 14.39034277 06
| Epoch (UTC): | 29 March 2026 04:57:38 |
| Eccentricity: | 0.0004204 |
| inclination: | 45.0382° |
| perigee height: | 759 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 179.2319° |
| argument of perigee: | 268.9357° |
| revolutions per day: | 14.39034277 |
| mean anomaly at epoch: | 91.1010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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