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 48129U 26145.35228595 +.00000000 +00000-0 +78192-5 0 00006
2 48129 53.1582 169.0065 0001007 102.3309 257.7805 15.31706496 09
| Epoch (UTC): | 25 May 2026 08:27:17 |
| Eccentricity: | 0.0001007 |
| inclination: | 53.1582° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 169.0065° |
| argument of perigee: | 102.3309° |
| revolutions per day: | 15.31706496 |
| mean anomaly at epoch: | 257.7805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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