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 23125U 26150.31446322 +.00000000 +00000-0 +12534-2 0 00002
2 23125 7.3936 252.4207 6434437 209.6298 89.4811 3.42972383 04
| Epoch (UTC): | 30 May 2026 07:32:49 |
| Eccentricity: | 0.6434437 |
| inclination: | 7.3936° |
| perigee height: | 244 km |
| apogee height: | 24147 km |
| right ascension of ascending node: | 252.4207° |
| argument of perigee: | 209.6298° |
| revolutions per day: | 3.42972383 |
| mean anomaly at epoch: | 89.4811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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