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 48994U 26145.53957462 +.00000000 +00000-0 +26731-3 0 00008
2 48994 87.9106 233.2716 0002115 96.7883 263.3488 13.16593493 09
| Epoch (UTC): | 25 May 2026 12:56:59 |
| Eccentricity: | 0.0002115 |
| inclination: | 87.9106° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2716° |
| argument of perigee: | 96.7883° |
| revolutions per day: | 13.16593493 |
| mean anomaly at epoch: | 263.3488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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