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 01002U 26075.85312769 +.00000000 +00000-0 +11447-3 0 00007
2 01002 32.1419 263.4537 0015766 297.2797 62.6094 9.88354955 06
| Epoch (UTC): | 16 March 2026 20:28:30 |
| Eccentricity: | 0.0015766 |
| inclination: | 32.1419° |
| perigee height: | 2779 km |
| apogee height: | 2808 km |
| right ascension of ascending node: | 263.4537° |
| argument of perigee: | 297.2797° |
| revolutions per day: | 9.88354955 |
| mean anomaly at epoch: | 62.6094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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