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 48130U 26145.36196157 +.00000000 +00000-0 +27396-4 0 00006
2 48130 53.1584 171.5761 0001254 87.8953 272.2192 15.31707228 05
| Epoch (UTC): | 25 May 2026 08:41:13 |
| Eccentricity: | 0.0001254 |
| inclination: | 53.1584° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 171.5761° |
| argument of perigee: | 87.8953° |
| revolutions per day: | 15.31707228 |
| mean anomaly at epoch: | 272.2192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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