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 25725U 26105.84288697 +.00000000 +00000-0 +22494-3 0 00004
2 25725 28.3222 275.0270 2385785 197.9393 152.0121 9.67484423 03
| Epoch (UTC): | 15 April 2026 20:13:45 |
| Eccentricity: | 0.2385785 |
| inclination: | 28.3222° |
| perigee height: | 706 km |
| apogee height: | 5145 km |
| right ascension of ascending node: | 275.0270° |
| argument of perigee: | 197.9393° |
| revolutions per day: | 9.67484423 |
| mean anomaly at epoch: | 152.0121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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