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 48993U 26145.27834066 +.00000000 +00000-0 -44155-4 0 00004
2 48993 87.9106 233.3234 0002008 97.1305 263.0054 13.16592900 07
| Epoch (UTC): | 25 May 2026 06:40:48 |
| Eccentricity: | 0.0002008 |
| inclination: | 87.9106° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.3234° |
| argument of perigee: | 97.1305° |
| revolutions per day: | 13.16592900 |
| mean anomaly at epoch: | 263.0054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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