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 48987U 26145.51899687 +.00000000 +00000-0 -19325-3 0 00004
2 48987 87.9093 233.2866 0002228 100.5216 259.6166 13.16593941 00
| Epoch (UTC): | 25 May 2026 12:27:21 |
| Eccentricity: | 0.0002228 |
| inclination: | 87.9093° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2866° |
| argument of perigee: | 100.5216° |
| revolutions per day: | 13.16593941 |
| mean anomaly at epoch: | 259.6166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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