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 36288U 26072.79858199 +.00000000 +00000-0 +13253-2 0 00009
2 36288 20.3432 343.0112 6957684 84.6325 344.5092 2.67592432 07
| Epoch (UTC): | 13 March 2026 19:09:57 |
| Eccentricity: | 0.6957684 |
| inclination: | 20.3432° |
| perigee height: | 289 km |
| apogee height: | 30786 km |
| right ascension of ascending node: | 343.0112° |
| argument of perigee: | 84.6325° |
| revolutions per day: | 2.67592432 |
| mean anomaly at epoch: | 344.5092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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