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 36605U 26102.52105047 +.00000000 +00000-0 +26693-4 0 00008
2 36605 97.4460 111.1625 0001674 88.6130 271.5297 15.19152778 02
| Epoch (UTC): | 12 April 2026 12:30:18 |
| Eccentricity: | 0.0001674 |
| inclination: | 97.4460° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 111.1625° |
| argument of perigee: | 88.6130° |
| revolutions per day: | 15.19152778 |
| mean anomaly at epoch: | 271.5297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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