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 26067.01981976 +.00000000 +00000-0 +15816-3 0 00008
2 16615 98.2232 84.7248 0010851 329.0675 58.4548 14.33291470 05
| Epoch (UTC): | 08 March 2026 00:28:32 |
| Eccentricity: | 0.0010851 |
| inclination: | 98.2232° |
| perigee height: | 773 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 84.7248° |
| argument of perigee: | 329.0675° |
| revolutions per day: | 14.33291470 |
| mean anomaly at epoch: | 58.4548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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