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 66409U 26144.91655022 +.00000000 +00000-0 +10460-3 0 00009
2 66409 98.2514 211.5684 0014490 47.5897 312.6521 14.50175951 09
| Epoch (UTC): | 24 May 2026 21:59:49 |
| Eccentricity: | 0.0014490 |
| inclination: | 98.2514° |
| perigee height: | 715 km |
| apogee height: | 735 km |
| right ascension of ascending node: | 211.5684° |
| argument of perigee: | 47.5897° |
| revolutions per day: | 14.50175951 |
| mean anomaly at epoch: | 312.6521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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