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 41473U 26145.58542318 +.00000000 +00000-0 +14806-3 0 00008
2 41473 97.9026 195.9715 0014461 310.3095 49.6850 14.76240296 01
| Epoch (UTC): | 25 May 2026 14:03:00 |
| Eccentricity: | 0.0014461 |
| inclination: | 97.9026° |
| perigee height: | 631 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 195.9715° |
| argument of perigee: | 310.3095° |
| revolutions per day: | 14.76240296 |
| mean anomaly at epoch: | 49.6850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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