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 56054U 26145.51482487 +.00000000 +00000-0 -33383-4 0 00005
2 56054 87.9250 248.4953 0001832 95.9273 264.2070 13.21825230 05
| Epoch (UTC): | 25 May 2026 12:21:20 |
| Eccentricity: | 0.0001832 |
| inclination: | 87.9250° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4953° |
| argument of perigee: | 95.9273° |
| revolutions per day: | 13.21825230 |
| mean anomaly at epoch: | 264.2070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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