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 53648U 26145.42197433 +.00000000 +00000-0 +99876-3 0 00002
2 53648 97.4500 25.4133 0001504 65.8398 294.2986 15.05584864 06
| Epoch (UTC): | 25 May 2026 10:07:38 |
| Eccentricity: | 0.0001504 |
| inclination: | 97.4500° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.4133° |
| argument of perigee: | 65.8398° |
| revolutions per day: | 15.05584864 |
| mean anomaly at epoch: | 294.2986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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