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 26061U 26038.88685515 +.00000000 +00000-0 +27958-3 0 00007
2 26061 100.2159 17.9754 0031143 238.9210 120.8917 14.44928203 00
| Epoch (UTC): | 07 February 2026 21:17:04 |
| Eccentricity: | 0.0031143 |
| inclination: | 100.2159° |
| perigee height: | 720 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 17.9754° |
| argument of perigee: | 238.9210° |
| revolutions per day: | 14.44928203 |
| mean anomaly at epoch: | 120.8917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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