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 23467U 26145.83177833 +.00000000 +00000-0 +00000-0 0 00003
2 23467 9.6978 13.3066 0003119 42.6034 299.2353 1.00268865 04
| Epoch (UTC): | 25 May 2026 19:57:45 |
| Eccentricity: | 0.0003119 |
| inclination: | 9.6978° |
| perigee height: | 35774 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 13.3066° |
| argument of perigee: | 42.6034° |
| revolutions per day: | 1.00268865 |
| mean anomaly at epoch: | 299.2353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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