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 53199U 26145.15331649 +.00000000 +00000-0 -94806-3 0 00001
2 53199 97.4452 206.2116 0001508 117.9147 242.2233 15.05717383 00
| Epoch (UTC): | 25 May 2026 03:40:46 |
| Eccentricity: | 0.0001508 |
| inclination: | 97.4452° |
| perigee height: | 548 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 206.2116° |
| argument of perigee: | 117.9147° |
| revolutions per day: | 15.05717383 |
| mean anomaly at epoch: | 242.2233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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