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 48860U 26145.67898985 +.00000000 +00000-0 +18982-3 0 00008
2 48860 34.9958 289.4116 0004275 243.4430 116.5840 15.02556648 02
| Epoch (UTC): | 25 May 2026 16:17:44 |
| Eccentricity: | 0.0004275 |
| inclination: | 34.9958° |
| perigee height: | 556 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 289.4116° |
| argument of perigee: | 243.4430° |
| revolutions per day: | 15.02556648 |
| mean anomaly at epoch: | 116.5840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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