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 43476U 18047A 26073.56884257 +.00006077 00000-0 +16462-3 0 02
2 43476 88.9911 210.9425 0013739 116.7180 345.1142 15.37507561435262
| Epoch (UTC): | 14 March 2026 13:39:07 |
| Eccentricity: | 0.0013739 |
| inclination: | 88.9911° |
| perigee height: | 444 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 210.9425° |
| argument of perigee: | 116.7180° |
| revolutions per day: | 15.37507561 |
| mean anomaly at epoch: | 345.1142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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