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 37948U 26145.31682316 +.00000000 +00000-0 +00000-0 0 00002
2 37948 47.7207 271.8266 0112255 220.8090 316.1246 1.00254419 08
| Epoch (UTC): | 25 May 2026 07:36:13 |
| Eccentricity: | 0.0112255 |
| inclination: | 47.7207° |
| perigee height: | 35318 km |
| apogee height: | 36265 km |
| right ascension of ascending node: | 271.8266° |
| argument of perigee: | 220.8090° |
| revolutions per day: | 1.00254419 |
| mean anomaly at epoch: | 316.1246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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