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 48986U 26145.53800644 +.00000000 +00000-0 +20676-3 0 00000
2 48986 87.9108 233.2778 0002107 98.1950 261.9420 13.16595545 02
| Epoch (UTC): | 25 May 2026 12:54:43 |
| Eccentricity: | 0.0002107 |
| inclination: | 87.9108° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2778° |
| argument of perigee: | 98.1950° |
| revolutions per day: | 13.16595545 |
| mean anomaly at epoch: | 261.9420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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