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 56325U 26145.45518549 +.00000000 +00000-0 +20681-4 0 00004
2 56325 97.4450 145.3805 0001974 89.8688 270.2765 15.05648593 01
| Epoch (UTC): | 25 May 2026 10:55:28 |
| Eccentricity: | 0.0001974 |
| inclination: | 97.4450° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 145.3805° |
| argument of perigee: | 89.8688° |
| revolutions per day: | 15.05648593 |
| mean anomaly at epoch: | 270.2765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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