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 65185U 26145.40612160 +.00000000 +00000-0 +52635-3 0 00000
2 65185 97.4498 17.8853 0002023 106.0361 254.1089 15.05658423 02
| Epoch (UTC): | 25 May 2026 09:44:48 |
| Eccentricity: | 0.0002023 |
| inclination: | 97.4498° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.8853° |
| argument of perigee: | 106.0361° |
| revolutions per day: | 15.05658423 |
| mean anomaly at epoch: | 254.1089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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