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 56070U 26145.36417663 +.00000000 +00000-0 -98382-4 0 00000
2 56070 87.8988 263.7600 0001879 102.4392 257.6948 13.15547635 09
| Epoch (UTC): | 25 May 2026 08:44:24 |
| Eccentricity: | 0.0001879 |
| inclination: | 87.8988° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7600° |
| argument of perigee: | 102.4392° |
| revolutions per day: | 13.15547635 |
| mean anomaly at epoch: | 257.6948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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