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 13637U 26150.52020323 +.00000000 +00000-0 +00000-0 0 00004
2 13637 12.4305 333.9646 0017254 198.3484 143.5307 0.97826590 06
| Epoch (UTC): | 30 May 2026 12:29:05 |
| Eccentricity: | 0.0017254 |
| inclination: | 12.4305° |
| perigee height: | 36412 km |
| apogee height: | 36560 km |
| right ascension of ascending node: | 333.9646° |
| argument of perigee: | 198.3484° |
| revolutions per day: | 0.97826590 |
| mean anomaly at epoch: | 143.5307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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