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 48784U 26145.57269131 +.00000000 +00000-0 +76424-4 0 00003
2 48784 87.9005 263.6766 0001927 113.3654 246.7679 13.15549944 06
| Epoch (UTC): | 25 May 2026 13:44:40 |
| Eccentricity: | 0.0001927 |
| inclination: | 87.9005° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.6766° |
| argument of perigee: | 113.3654° |
| revolutions per day: | 13.15549944 |
| mean anomaly at epoch: | 246.7679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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