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 43802U 26145.58334904 +.00000000 +00000-0 +56106-3 0 00005
2 43802 96.9179 194.3240 0004019 207.9694 152.1369 15.97877566 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0004019 |
| inclination: | 96.9179° |
| perigee height: | 278 km |
| apogee height: | 283 km |
| right ascension of ascending node: | 194.3240° |
| argument of perigee: | 207.9694° |
| revolutions per day: | 15.97877566 |
| mean anomaly at epoch: | 152.1369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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