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 60454U 26145.59123453 +.00000000 +00000-0 +46788-3 0 00008
2 60454 37.3802 200.6632 0001472 112.4741 247.6179 15.47639497 08
| Epoch (UTC): | 25 May 2026 14:11:22 |
| Eccentricity: | 0.0001472 |
| inclination: | 37.3802° |
| perigee height: | 423 km |
| apogee height: | 425 km |
| right ascension of ascending node: | 200.6632° |
| argument of perigee: | 112.4741° |
| revolutions per day: | 15.47639497 |
| mean anomaly at epoch: | 247.6179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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