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 26129.85887622 +.00000000 +00000-0 +32839-4 0 00003
2 14974 82.9366 245.1958 0043518 268.7501 213.9375 13.77161935 08
| Epoch (UTC): | 09 May 2026 20:36:46 |
| Eccentricity: | 0.0043518 |
| inclination: | 82.9366° |
| perigee height: | 942 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 245.1958° |
| argument of perigee: | 268.7501° |
| revolutions per day: | 13.77161935 |
| mean anomaly at epoch: | 213.9375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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