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 48412U 26144.81133691 +.00000000 +00000-0 +79427-4 0 00004
2 48412 53.1580 302.4158 0000798 94.7917 265.3176 15.31702545 00
| Epoch (UTC): | 24 May 2026 19:28:19 |
| Eccentricity: | 0.0000798 |
| inclination: | 53.1580° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 302.4158° |
| argument of perigee: | 94.7917° |
| revolutions per day: | 15.31702545 |
| mean anomaly at epoch: | 265.3176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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