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 26387U 26017.86884083 +.00000000 +00000-0 +15172-3 0 00009
2 26387 97.8213 354.8947 0025089 25.8625 334.3832 14.73615914 07
| Epoch (UTC): | 17 January 2026 20:51:07 |
| Eccentricity: | 0.0025089 |
| inclination: | 97.8213° |
| perigee height: | 632 km |
| apogee height: | 667 km |
| right ascension of ascending node: | 354.8947° |
| argument of perigee: | 25.8625° |
| revolutions per day: | 14.73615914 |
| mean anomaly at epoch: | 334.3832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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