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 36131U 26145.00781574 +.00000000 +00000-0 +00000-0 0 00007
2 36131 0.0128 97.4502 0000327 275.2792 129.9570 1.00269038 02
| Epoch (UTC): | 25 May 2026 00:11:15 |
| Eccentricity: | 0.0000327 |
| inclination: | 0.0128° |
| perigee height: | 35786 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 97.4502° |
| argument of perigee: | 275.2792° |
| revolutions per day: | 1.00269038 |
| mean anomaly at epoch: | 129.9570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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