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 41330U 26145.29143597 +.00000000 +00000-0 +00000-0 0 00002
2 41330 65.0358 313.7919 0010420 196.8088 163.1523 2.13102636 05
| Epoch (UTC): | 25 May 2026 06:59:40 |
| Eccentricity: | 0.0010420 |
| inclination: | 65.0358° |
| perigee height: | 19103 km |
| apogee height: | 19156 km |
| right ascension of ascending node: | 313.7919° |
| argument of perigee: | 196.8088° |
| revolutions per day: | 2.13102636 |
| mean anomaly at epoch: | 163.1523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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