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 56048U 26145.52850461 +.00000000 +00000-0 -11820-3 0 00001
2 56048 87.9106 233.2720 0002496 113.4685 246.6709 13.16593111 09
| Epoch (UTC): | 25 May 2026 12:41:02 |
| Eccentricity: | 0.0002496 |
| inclination: | 87.9106° |
| perigee height: | 1196 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 233.2720° |
| argument of perigee: | 113.4685° |
| revolutions per day: | 13.16593111 |
| mean anomaly at epoch: | 246.6709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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