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 26068.43401740 +.00000000 +00000-0 +47043-3 0 00009
2 14690 63.2981 74.2458 0637146 123.1893 243.1939 14.13401649 09
| Epoch (UTC): | 09 March 2026 10:24:59 |
| Eccentricity: | 0.0637146 |
| inclination: | 63.2981° |
| perigee height: | 387 km |
| apogee height: | 1308 km |
| right ascension of ascending node: | 74.2458° |
| argument of perigee: | 123.1893° |
| revolutions per day: | 14.13401649 |
| mean anomaly at epoch: | 243.1939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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