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 48076U 26145.22254558 +.00000000 +00000-0 -55314-3 0 00001
2 48076 87.8951 324.7868 0002015 90.6624 269.4736 13.13468842 05
| Epoch (UTC): | 25 May 2026 05:20:27 |
| Eccentricity: | 0.0002015 |
| inclination: | 87.8951° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7868° |
| argument of perigee: | 90.6624° |
| revolutions per day: | 13.13468842 |
| mean anomaly at epoch: | 269.4736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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