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 26064.66248920 +.00000000 +00000-0 +15277-3 0 00002
2 16615 98.2232 82.4851 0010969 336.4334 134.6634 14.33289391 06
| Epoch (UTC): | 05 March 2026 15:53:59 |
| Eccentricity: | 0.0010969 |
| inclination: | 98.2232° |
| perigee height: | 773 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 82.4851° |
| argument of perigee: | 336.4334° |
| revolutions per day: | 14.33289391 |
| mean anomaly at epoch: | 134.6634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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