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 41339U 26150.85124727 +.00000000 +00000-0 +34794-3 0 00003
2 41339 31.0043 84.3071 0009321 250.2730 109.6906 15.18397542 06
| Epoch (UTC): | 30 May 2026 20:25:47 |
| Eccentricity: | 0.0009321 |
| inclination: | 31.0043° |
| perigee height: | 504 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 84.3071° |
| argument of perigee: | 250.2730° |
| revolutions per day: | 15.18397542 |
| mean anomaly at epoch: | 109.6906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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