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 56356U 26145.23500434 +.00000000 +00000-0 -47244-3 0 00002
2 56356 97.4489 146.2867 0001544 67.8155 292.3236 15.05685648 03
| Epoch (UTC): | 25 May 2026 05:38:24 |
| Eccentricity: | 0.0001544 |
| inclination: | 97.4489° |
| perigee height: | 548 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 146.2867° |
| argument of perigee: | 67.8155° |
| revolutions per day: | 15.05685648 |
| mean anomaly at epoch: | 292.3236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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