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 25983U 26087.94713082 +.00000000 +00000-0 +36531-3 0 00008
2 25983 45.0278 84.2474 0007115 41.7874 318.3518 14.40829030 09
| Epoch (UTC): | 28 March 2026 22:43:52 |
| Eccentricity: | 0.0007115 |
| inclination: | 45.0278° |
| perigee height: | 751 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 84.2474° |
| argument of perigee: | 41.7874° |
| revolutions per day: | 14.40829030 |
| mean anomaly at epoch: | 318.3518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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