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 65435U 26145.33433443 +.00000000 +00000-0 +27813-3 0 00005
2 65435 97.4488 359.6036 0002026 92.9749 267.1710 15.05657650 01
| Epoch (UTC): | 25 May 2026 08:01:26 |
| Eccentricity: | 0.0002026 |
| inclination: | 97.4488° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.6036° |
| argument of perigee: | 92.9749° |
| revolutions per day: | 15.05657650 |
| mean anomaly at epoch: | 267.1710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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