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 35869U 26106.43284419 +.00000000 +00000-0 +30495-4 0 00009
2 35869 98.7347 68.7339 0005397 114.9087 245.2653 14.23201071 09
| Epoch (UTC): | 16 April 2026 10:23:17 |
| Eccentricity: | 0.0005397 |
| inclination: | 98.7347° |
| perigee height: | 811 km |
| apogee height: | 818 km |
| right ascension of ascending node: | 68.7339° |
| argument of perigee: | 114.9087° |
| revolutions per day: | 14.23201071 |
| mean anomaly at epoch: | 245.2653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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