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 26111.55803116 +.00000000 +00000-0 +51283-6 0 00002
2 00059 28.2497 54.5015 0188976 200.3967 158.8947 13.53167270 01
| Epoch (UTC): | 21 April 2026 13:23:33 |
| Eccentricity: | 0.0188976 |
| inclination: | 28.2497° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 54.5015° |
| argument of perigee: | 200.3967° |
| revolutions per day: | 13.53167270 |
| mean anomaly at epoch: | 158.8947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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