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 26064.21674638 +.00000000 +00000-0 +86017-4 0 00001
2 14453 81.1674 143.0132 0103405 211.8003 147.6907 14.25438006 05
| Epoch (UTC): | 05 March 2026 05:12:06 |
| Eccentricity: | 0.0103405 |
| inclination: | 81.1674° |
| perigee height: | 733 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 143.0132° |
| argument of perigee: | 211.8003° |
| revolutions per day: | 14.25438006 |
| mean anomaly at epoch: | 147.6907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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