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 26104.25490231 +.00000000 +00000-0 +23426-4 0 00007
2 00059 28.2474 92.0286 0189019 139.0816 222.4082 13.53167091 02
| Epoch (UTC): | 14 April 2026 06:07:03 |
| Eccentricity: | 0.0189019 |
| inclination: | 28.2474° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 92.0286° |
| argument of perigee: | 139.0816° |
| revolutions per day: | 13.53167091 |
| mean anomaly at epoch: | 222.4082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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