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 56970U 26145.35390405 +.00000000 +00000-0 +37313-3 0 00007
2 56970 97.6259 288.6926 0009477 44.0913 316.1085 15.36886243 06
| Epoch (UTC): | 25 May 2026 08:29:37 |
| Eccentricity: | 0.0009477 |
| inclination: | 97.6259° |
| perigee height: | 449 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 288.6926° |
| argument of perigee: | 44.0913° |
| revolutions per day: | 15.36886243 |
| mean anomaly at epoch: | 316.1085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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