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 26127.89722927 +.00000000 +00000-0 +48215-4 0 00006
2 14974 82.9364 246.6556 0043518 274.4207 208.3394 13.77161807 00
| Epoch (UTC): | 07 May 2026 21:32:00 |
| Eccentricity: | 0.0043518 |
| inclination: | 82.9364° |
| perigee height: | 942 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 246.6556° |
| argument of perigee: | 274.4207° |
| revolutions per day: | 13.77161807 |
| mean anomaly at epoch: | 208.3394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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