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 26861U 26081.23489240 +.00000000 +00000-0 +81427-4 0 00001
2 26861 98.8053 75.5818 0099428 240.4621 118.6620 14.29679096 00
| Epoch (UTC): | 22 March 2026 05:38:14 |
| Eccentricity: | 0.0099428 |
| inclination: | 98.8053° |
| perigee height: | 722 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 75.5818° |
| argument of perigee: | 240.4621° |
| revolutions per day: | 14.29679096 |
| mean anomaly at epoch: | 118.6620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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