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 48789U 26145.57887190 +.00000000 +00000-0 -14506-3 0 00002
2 48789 87.9000 263.6931 0001709 97.4248 262.7076 13.15547586 08
| Epoch (UTC): | 25 May 2026 13:53:34 |
| Eccentricity: | 0.0001709 |
| inclination: | 87.9000° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6931° |
| argument of perigee: | 97.4248° |
| revolutions per day: | 13.15547586 |
| mean anomaly at epoch: | 262.7076° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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