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 48984U 26145.25458398 +.00000000 +00000-0 +10979-3 0 00007
2 48984 87.9106 233.3278 0002033 102.1834 257.9525 13.16593235 04
| Epoch (UTC): | 25 May 2026 06:06:36 |
| Eccentricity: | 0.0002033 |
| inclination: | 87.9106° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.3278° |
| argument of perigee: | 102.1834° |
| revolutions per day: | 13.16593235 |
| mean anomaly at epoch: | 257.9525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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