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 57463U 26145.66668980 +.00000000 +00000-0 +24100-1 0 00003
2 57463 42.9995 260.2177 0001336 286.0778 58.3100 15.48293530 08
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001336 |
| inclination: | 42.9995° |
| perigee height: | 421 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 260.2177° |
| argument of perigee: | 286.0778° |
| revolutions per day: | 15.48293530 |
| mean anomaly at epoch: | 58.3100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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