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 55453U 26145.58094264 +.00000000 +00000-0 +53187-4 0 00009
2 55453 43.0038 254.3019 0001647 262.4560 97.6104 15.27578274 04
| Epoch (UTC): | 25 May 2026 13:56:33 |
| Eccentricity: | 0.0001647 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.3019° |
| argument of perigee: | 262.4560° |
| revolutions per day: | 15.27578274 |
| mean anomaly at epoch: | 97.6104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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