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 16615U 26067.59525748 +.00000000 +00000-0 +15448-3 0 00003
2 16615 98.2232 85.2715 0010821 327.3004 147.6765 14.33291904 08
| Epoch (UTC): | 08 March 2026 14:17:10 |
| Eccentricity: | 0.0010821 |
| inclination: | 98.2232° |
| perigee height: | 773 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 85.2715° |
| argument of perigee: | 327.3004° |
| revolutions per day: | 14.33291904 |
| mean anomaly at epoch: | 147.6765° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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