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 65087U 26145.09789516 +.00000000 +00000-0 +30107-3 0 00006
2 65087 53.1592 32.0826 0001063 96.1709 263.9413 15.30204895 01
| Epoch (UTC): | 25 May 2026 02:20:58 |
| Eccentricity: | 0.0001063 |
| inclination: | 53.1592° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 32.0826° |
| argument of perigee: | 96.1709° |
| revolutions per day: | 15.30204895 |
| mean anomaly at epoch: | 263.9413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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