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 65213U 26145.41958271 +.00000000 +00000-0 +60889-3 0 00009
2 65213 53.1598 155.9339 0001422 94.7667 265.3498 15.34389040 07
| Epoch (UTC): | 25 May 2026 10:04:11 |
| Eccentricity: | 0.0001422 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 155.9339° |
| argument of perigee: | 94.7667° |
| revolutions per day: | 15.34389040 |
| mean anomaly at epoch: | 265.3498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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