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 11112U 26088.20027066 +.00000000 +00000-0 +11010-3 0 00002
2 11112 74.0322 21.7384 0032096 119.6542 240.7816 14.38778843 00
| Epoch (UTC): | 29 March 2026 04:48:23 |
| Eccentricity: | 0.0032096 |
| inclination: | 74.0322° |
| perigee height: | 740 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 21.7384° |
| argument of perigee: | 119.6542° |
| revolutions per day: | 14.38778843 |
| mean anomaly at epoch: | 240.7816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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