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 00059U 26048.33439501 +.00000000 +00000-0 +64232-4 0 00006
2 00059 28.2499 19.3760 0188877 29.6388 331.4715 13.53161894 06
| Epoch (UTC): | 17 February 2026 08:01:31 |
| Eccentricity: | 0.0188877 |
| inclination: | 28.2499° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 19.3760° |
| argument of perigee: | 29.6388° |
| revolutions per day: | 13.53161894 |
| mean anomaly at epoch: | 331.4715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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