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 61623U 26145.24204286 +.00000000 +00000-0 -66482-5 0 00009
2 61623 43.0024 85.6814 0001142 262.7290 97.3432 15.27580349 03
| Epoch (UTC): | 25 May 2026 05:48:32 |
| Eccentricity: | 0.0001142 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 85.6814° |
| argument of perigee: | 262.7290° |
| revolutions per day: | 15.27580349 |
| mean anomaly at epoch: | 97.3432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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