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 26074.57563075 +.00000000 +00000-0 +10438-3 0 00008
2 16615 98.2226 91.9036 0010488 304.7722 167.1169 14.33296517 06
| Epoch (UTC): | 15 March 2026 13:48:54 |
| Eccentricity: | 0.0010488 |
| inclination: | 98.2226° |
| perigee height: | 773 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 91.9036° |
| argument of perigee: | 304.7722° |
| revolutions per day: | 14.33296517 |
| mean anomaly at epoch: | 167.1169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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