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 48996U 26145.54275681 +.00000000 +00000-0 +27427-3 0 00000
2 48996 87.9110 233.2696 0002095 106.9457 253.1904 13.16595859 09
| Epoch (UTC): | 25 May 2026 13:01:34 |
| Eccentricity: | 0.0002095 |
| inclination: | 87.9110° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2696° |
| argument of perigee: | 106.9457° |
| revolutions per day: | 13.16595859 |
| mean anomaly at epoch: | 253.1904° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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