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 65494U 26145.64310346 +.00000000 +00000-0 +58539-3 0 00009
2 65494 53.1595 272.7330 0000974 68.8171 291.2935 15.34388634 09
| Epoch (UTC): | 25 May 2026 15:26:04 |
| Eccentricity: | 0.0000974 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 272.7330° |
| argument of perigee: | 68.8171° |
| revolutions per day: | 15.34388634 |
| mean anomaly at epoch: | 291.2935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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