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 10461U 26068.36080476 +.00000000 +00000-0 +85870-4 0 00003
2 10461 82.9533 166.9151 0032428 225.4785 198.9652 13.77136634 06
| Epoch (UTC): | 09 March 2026 08:39:33 |
| Eccentricity: | 0.0032428 |
| inclination: | 82.9533° |
| perigee height: | 950 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 166.9151° |
| argument of perigee: | 225.4785° |
| revolutions per day: | 13.77136634 |
| mean anomaly at epoch: | 198.9652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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