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 56351U 26145.43715352 +.00000000 +00000-0 +20779-4 0 00000
2 56351 97.4486 146.4736 0001893 87.3249 272.8195 15.05652484 09
| Epoch (UTC): | 25 May 2026 10:29:30 |
| Eccentricity: | 0.0001893 |
| inclination: | 97.4486° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.4736° |
| argument of perigee: | 87.3249° |
| revolutions per day: | 15.05652484 |
| mean anomaly at epoch: | 272.8195° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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