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 14690U 26067.44349961 +.00000000 +00000-0 +65513-3 0 00007
2 14690 63.2979 77.1335 0637252 123.1726 243.2128 14.13387303 06
| Epoch (UTC): | 08 March 2026 10:38:38 |
| Eccentricity: | 0.0637252 |
| inclination: | 63.2979° |
| perigee height: | 387 km |
| apogee height: | 1308 km |
| right ascension of ascending node: | 77.1335° |
| argument of perigee: | 123.1726° |
| revolutions per day: | 14.13387303 |
| mean anomaly at epoch: | 243.2128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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