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 40099U 26143.28633777 +.00000000 +00000-0 +00000-0 0 00004
2 40099 5.4380 75.5399 0001943 70.2520 117.8057 0.96773065 07
| Epoch (UTC): | 23 May 2026 06:52:19 |
| Eccentricity: | 0.0001943 |
| inclination: | 5.4380° |
| perigee height: | 36788 km |
| apogee height: | 36805 km |
| right ascension of ascending node: | 75.5399° |
| argument of perigee: | 70.2520° |
| revolutions per day: | 0.96773065 |
| mean anomaly at epoch: | 117.8057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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