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 55350U 26145.62128221 +.00000000 +00000-0 +10767-4 0 00008
2 55350 43.0048 228.5472 0002086 279.9864 80.0752 15.27579176 02
| Epoch (UTC): | 25 May 2026 14:54:38 |
| Eccentricity: | 0.0002086 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 228.5472° |
| argument of perigee: | 279.9864° |
| revolutions per day: | 15.27579176 |
| mean anomaly at epoch: | 80.0752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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