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 26104.03505700 +.00000000 +00000-0 +24762-3 0 00008
2 25984 45.0380 104.1052 0003879 335.4212 24.6451 14.39076280 02
| Epoch (UTC): | 14 April 2026 00:50:28 |
| Eccentricity: | 0.0003879 |
| inclination: | 45.0380° |
| perigee height: | 759 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 104.1052° |
| argument of perigee: | 335.4212° |
| revolutions per day: | 14.39076280 |
| mean anomaly at epoch: | 24.6451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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