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 14453U 26065.48024196 +.00000000 +00000-0 +82036-4 0 00006
2 14453 81.1673 141.7408 0103473 208.1379 151.4187 14.25438412 09
| Epoch (UTC): | 06 March 2026 11:31:32 |
| Eccentricity: | 0.0103473 |
| inclination: | 81.1673° |
| perigee height: | 733 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 141.7408° |
| argument of perigee: | 208.1379° |
| revolutions per day: | 14.25438412 |
| mean anomaly at epoch: | 151.4187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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