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 65274U 26145.41579156 +.00000000 +00000-0 +40681-3 0 00005
2 65274 97.4504 197.8801 0001546 122.4221 237.7156 15.05659788 04
| Epoch (UTC): | 25 May 2026 09:58:44 |
| Eccentricity: | 0.0001546 |
| inclination: | 97.4504° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 197.8801° |
| argument of perigee: | 122.4221° |
| revolutions per day: | 15.05659788 |
| mean anomaly at epoch: | 237.7156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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