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 10656U 26065.41824367 +.00000000 +00000-0 +45565-3 0 00003
2 10656 101.8546 39.6321 0077375 315.3796 214.9598 12.37110922 08
| Epoch (UTC): | 06 March 2026 10:02:16 |
| Eccentricity: | 0.0077375 |
| inclination: | 101.8546° |
| perigee height: | 1458 km |
| apogee height: | 1580 km |
| right ascension of ascending node: | 39.6321° |
| argument of perigee: | 315.3796° |
| revolutions per day: | 12.37110922 |
| mean anomaly at epoch: | 214.9598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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