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 04256U 26031.90652686 +.00000000 +00000-0 +13224-3 0 00009
2 04256 70.0078 257.7716 0022164 246.3717 113.5064 13.99153437 06
| Epoch (UTC): | 31 January 2026 21:45:23 |
| Eccentricity: | 0.0022164 |
| inclination: | 70.0078° |
| perigee height: | 881 km |
| apogee height: | 913 km |
| right ascension of ascending node: | 257.7716° |
| argument of perigee: | 246.3717° |
| revolutions per day: | 13.99153437 |
| mean anomaly at epoch: | 113.5064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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