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 36519U 26109.75073750 +.00000000 +00000-0 +10190-4 0 00004
2 36519 82.9569 292.6532 0034893 293.0977 77.2680 13.71661724 06
| Epoch (UTC): | 19 April 2026 18:01:03 |
| Eccentricity: | 0.0034893 |
| inclination: | 82.9569° |
| perigee height: | 968 km |
| apogee height: | 1019 km |
| right ascension of ascending node: | 292.6532° |
| argument of perigee: | 293.0977° |
| revolutions per day: | 13.71661724 |
| mean anomaly at epoch: | 77.2680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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