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 65436U 26145.10407885 +.00000000 +00000-0 +15200-3 0 00009
2 65436 97.5159 359.9476 0002390 86.1150 274.0350 15.04838965 00
| Epoch (UTC): | 25 May 2026 02:29:52 |
| Eccentricity: | 0.0002390 |
| inclination: | 97.5159° |
| perigee height: | 550 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 359.9476° |
| argument of perigee: | 86.1150° |
| revolutions per day: | 15.04838965 |
| mean anomaly at epoch: | 274.0350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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