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 23087U 26106.92994133 +.00000000 +00000-0 +20349-3 0 00009
2 23087 71.0513 95.0902 0009898 319.3996 40.6388 14.14381211 03
| Epoch (UTC): | 16 April 2026 22:19:06 |
| Eccentricity: | 0.0009898 |
| inclination: | 71.0513° |
| perigee height: | 837 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 95.0902° |
| argument of perigee: | 319.3996° |
| revolutions per day: | 14.14381211 |
| mean anomaly at epoch: | 40.6388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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