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 16275U 26156.93953703 +.00000000 +00000-0 +00000-0 0 00003
2 16275 13.3696 340.2160 0004207 326.7251 25.6200 0.99936643 00
| Epoch (UTC): | 05 June 2026 22:32:55 |
| Eccentricity: | 0.0004207 |
| inclination: | 13.3696° |
| perigee height: | 35863 km |
| apogee height: | 35899 km |
| right ascension of ascending node: | 340.2160° |
| argument of perigee: | 326.7251° |
| revolutions per day: | 0.99936643 |
| mean anomaly at epoch: | 25.6200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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