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 48390U 26145.49604140 +.00000000 +00000-0 +35051-4 0 00001
2 48390 53.1599 335.4314 0003405 84.6734 275.4656 15.31694957 00
| Epoch (UTC): | 25 May 2026 11:54:17 |
| Eccentricity: | 0.0003405 |
| inclination: | 53.1599° |
| perigee height: | 468 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 335.4314° |
| argument of perigee: | 84.6734° |
| revolutions per day: | 15.31694957 |
| mean anomaly at epoch: | 275.4656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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