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 61232U 26145.56786920 +.00000000 +00000-0 +34083-3 0 00009
2 61232 97.3506 241.1315 0006128 200.0955 160.0068 15.72314067 08
| Epoch (UTC): | 25 May 2026 13:37:43 |
| Eccentricity: | 0.0006128 |
| inclination: | 97.3506° |
| perigee height: | 348 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 241.1315° |
| argument of perigee: | 200.0955° |
| revolutions per day: | 15.72314067 |
| mean anomaly at epoch: | 160.0068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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