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 65858U 26145.14912258 +.00000000 +00000-0 +41720-3 0 00002
2 65858 53.1597 298.9059 0001044 103.8620 256.2498 15.30210176 07
| Epoch (UTC): | 25 May 2026 03:34:44 |
| Eccentricity: | 0.0001044 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 298.9059° |
| argument of perigee: | 103.8620° |
| revolutions per day: | 15.30210176 |
| mean anomaly at epoch: | 256.2498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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