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 26039.60084053 +.00000000 +00000-0 -53734-4 0 00006
2 23087 71.0500 235.9562 0006612 68.6040 291.5787 14.14363676 06
| Epoch (UTC): | 08 February 2026 14:25:12 |
| Eccentricity: | 0.0006612 |
| inclination: | 71.0500° |
| perigee height: | 840 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 235.9562° |
| argument of perigee: | 68.6040° |
| revolutions per day: | 14.14363676 |
| mean anomaly at epoch: | 291.5787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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