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 65799U 26145.55091772 +.00000000 +00000-0 +64013-4 0 00001
2 65799 97.4485 8.3039 0002496 85.6893 274.4619 15.05652804 07
| Epoch (UTC): | 25 May 2026 13:13:19 |
| Eccentricity: | 0.0002496 |
| inclination: | 97.4485° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.3039° |
| argument of perigee: | 85.6893° |
| revolutions per day: | 15.05652804 |
| mean anomaly at epoch: | 274.4619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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