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 14974U 26088.08165117 +.00000000 +00000-0 -53548-4 0 00001
2 14974 82.9313 276.2983 0045460 27.3906 89.8957 13.77162680 03
| Epoch (UTC): | 29 March 2026 01:57:34 |
| Eccentricity: | 0.0045460 |
| inclination: | 82.9313° |
| perigee height: | 941 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 276.2983° |
| argument of perigee: | 27.3906° |
| revolutions per day: | 13.77162680 |
| mean anomaly at epoch: | 89.8957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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