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 65097U 26145.10356448 +.00000000 +00000-0 +93624-3 0 00006
2 65097 53.1602 29.2701 0001090 85.4896 274.6234 15.42188897 08
| Epoch (UTC): | 25 May 2026 02:29:07 |
| Eccentricity: | 0.0001090 |
| inclination: | 53.1602° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 29.2701° |
| argument of perigee: | 85.4896° |
| revolutions per day: | 15.42188897 |
| mean anomaly at epoch: | 274.6234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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