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 14454U 26088.24323072 +.00000000 +00000-0 +63455-4 0 00005
2 14454 81.1587 86.9040 0095682 95.9652 276.8488 14.26387043 04
| Epoch (UTC): | 29 March 2026 05:50:15 |
| Eccentricity: | 0.0095682 |
| inclination: | 81.1587° |
| perigee height: | 735 km |
| apogee height: | 873 km |
| right ascension of ascending node: | 86.9040° |
| argument of perigee: | 95.9652° |
| revolutions per day: | 14.26387043 |
| mean anomaly at epoch: | 276.8488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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