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 26048.92461794 +.00000000 +00000-0 +58542-4 0 00007
2 00059 28.2498 16.3433 0188882 34.5937 326.6740 13.53161899 09
| Epoch (UTC): | 17 February 2026 22:11:26 |
| Eccentricity: | 0.0188882 |
| inclination: | 28.2498° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 16.3433° |
| argument of perigee: | 34.5937° |
| revolutions per day: | 13.53161899 |
| mean anomaly at epoch: | 326.6740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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