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 41337U 26107.30096212 +.00000000 +00000-0 +10356-3 0 00008
2 41337 30.9981 107.3284 0009520 359.4499 0.6127 15.10234836 03
| Epoch (UTC): | 17 April 2026 07:13:23 |
| Eccentricity: | 0.0009520 |
| inclination: | 30.9981° |
| perigee height: | 529 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 107.3284° |
| argument of perigee: | 359.4499° |
| revolutions per day: | 15.10234836 |
| mean anomaly at epoch: | 0.6127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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