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 53674U 26145.40534231 +.00000000 +00000-0 -11070-3 0 00001
2 53674 97.4477 25.3449 0002546 75.3081 284.8428 15.05660898 07
| Epoch (UTC): | 25 May 2026 09:43:41 |
| Eccentricity: | 0.0002546 |
| inclination: | 97.4477° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.3449° |
| argument of perigee: | 75.3081° |
| revolutions per day: | 15.05660898 |
| mean anomaly at epoch: | 284.8428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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