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 65395U 26145.35490141 +.00000000 +00000-0 +26770-3 0 00001
2 65395 97.4471 16.6843 0002315 75.5337 284.6147 15.05660987 00
| Epoch (UTC): | 25 May 2026 08:31:03 |
| Eccentricity: | 0.0002315 |
| inclination: | 97.4471° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.6843° |
| argument of perigee: | 75.5337° |
| revolutions per day: | 15.05660987 |
| mean anomaly at epoch: | 284.6147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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