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 65025U 26145.15812390 +.00000000 +00000-0 +16722-2 0 00008
2 65025 53.1612 298.5776 0000849 71.3349 288.7745 15.33613224 01
| Epoch (UTC): | 25 May 2026 03:47:41 |
| Eccentricity: | 0.0000849 |
| inclination: | 53.1612° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 298.5776° |
| argument of perigee: | 71.3349° |
| revolutions per day: | 15.33613224 |
| mean anomaly at epoch: | 288.7745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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