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 48274U 26132.51920400 +.00000000 +00000-0 +13837-3 0 00008
2 48274 41.4671 178.9319 0004229 292.2546 67.7845 15.62150141 08
| Epoch (UTC): | 12 May 2026 12:27:39 |
| Eccentricity: | 0.0004229 |
| inclination: | 41.4671° |
| perigee height: | 379 km |
| apogee height: | 384 km |
| right ascension of ascending node: | 178.9319° |
| argument of perigee: | 292.2546° |
| revolutions per day: | 15.62150141 |
| mean anomaly at epoch: | 67.7845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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