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 48992U 26145.51740431 +.00000000 +00000-0 +91685-4 0 00001
2 48992 87.9096 233.2892 0002195 92.9492 267.1890 13.16595702 06
| Epoch (UTC): | 25 May 2026 12:25:03 |
| Eccentricity: | 0.0002195 |
| inclination: | 87.9096° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2892° |
| argument of perigee: | 92.9492° |
| revolutions per day: | 13.16595702 |
| mean anomaly at epoch: | 267.1890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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