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 53055U 26145.49391727 +.00000000 +00000-0 +12683-4 0 00005
2 53055 97.4477 326.4923 0001448 94.3098 265.8295 15.05650920 07
| Epoch (UTC): | 25 May 2026 11:51:14 |
| Eccentricity: | 0.0001448 |
| inclination: | 97.4477° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 326.4923° |
| argument of perigee: | 94.3098° |
| revolutions per day: | 15.05650920 |
| mean anomaly at epoch: | 265.8295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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