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 53156U 26145.41837676 +.00000000 +00000-0 -30965-4 0 00001
2 53156 53.2117 179.5472 0001248 100.7117 259.4015 15.08839207 07
| Epoch (UTC): | 25 May 2026 10:02:27 |
| Eccentricity: | 0.0001248 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 179.5472° |
| argument of perigee: | 100.7117° |
| revolutions per day: | 15.08839207 |
| mean anomaly at epoch: | 259.4015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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