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 26088.20913253 +.00000000 +00000-0 +19149-3 0 00005
2 26387 97.8330 62.7789 0024822 153.1425 207.1075 14.73822624 07
| Epoch (UTC): | 29 March 2026 05:01:09 |
| Eccentricity: | 0.0024822 |
| inclination: | 97.8330° |
| perigee height: | 631 km |
| apogee height: | 666 km |
| right ascension of ascending node: | 62.7789° |
| argument of perigee: | 153.1425° |
| revolutions per day: | 14.73822624 |
| mean anomaly at epoch: | 207.1075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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