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 14760U 26088.20306270 +.00000000 +00000-0 +97115-4 0 00002
2 14760 74.0452 355.4345 0027073 149.4975 210.7761 14.37184463 04
| Epoch (UTC): | 29 March 2026 04:52:24 |
| Eccentricity: | 0.0027073 |
| inclination: | 74.0452° |
| perigee height: | 748 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 355.4345° |
| argument of perigee: | 149.4975° |
| revolutions per day: | 14.37184463 |
| mean anomaly at epoch: | 210.7761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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