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 26064.01805641 +.00000000 +00000-0 +14079-3 0 00009
2 16615 98.2233 81.8728 0011015 338.4332 49.4165 14.33288695 04
| Epoch (UTC): | 05 March 2026 00:26:00 |
| Eccentricity: | 0.0011015 |
| inclination: | 98.2233° |
| perigee height: | 773 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 81.8728° |
| argument of perigee: | 338.4332° |
| revolutions per day: | 14.33288695 |
| mean anomaly at epoch: | 49.4165° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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