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 65812U 26145.11617112 +.00000000 +00000-0 +32413-3 0 00009
2 65812 97.4519 7.9696 0001508 57.7146 302.4228 15.05661632 06
| Epoch (UTC): | 25 May 2026 02:47:17 |
| Eccentricity: | 0.0001508 |
| inclination: | 97.4519° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 7.9696° |
| argument of perigee: | 57.7146° |
| revolutions per day: | 15.05661632 |
| mean anomaly at epoch: | 302.4228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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