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 53453U 26145.61171156 +.00000000 +00000-0 +66577-3 0 00003
2 53453 97.5552 275.5061 0000606 174.5848 185.5420 15.68337493 04
| Epoch (UTC): | 25 May 2026 14:40:51 |
| Eccentricity: | 0.0000606 |
| inclination: | 97.5552° |
| perigee height: | 363 km |
| apogee height: | 364 km |
| right ascension of ascending node: | 275.5061° |
| argument of perigee: | 174.5848° |
| revolutions per day: | 15.68337493 |
| mean anomaly at epoch: | 185.5420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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