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 40275U 26145.44642007 +.00000000 +00000-0 +11979-3 0 00006
2 40275 100.7694 296.3446 0005875 238.3069 121.7470 13.15530512 05
| Epoch (UTC): | 25 May 2026 10:42:50 |
| Eccentricity: | 0.0005875 |
| inclination: | 100.7694° |
| perigee height: | 1197 km |
| apogee height: | 1206 km |
| right ascension of ascending node: | 296.3446° |
| argument of perigee: | 238.3069° |
| revolutions per day: | 13.15530512 |
| mean anomaly at epoch: | 121.7470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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