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 48861U 26145.59112112 +.00000000 +00000-0 +18957-3 0 00003
2 48861 34.9955 289.5808 0004702 248.9731 111.0474 15.02546314 00
| Epoch (UTC): | 25 May 2026 14:11:12 |
| Eccentricity: | 0.0004702 |
| inclination: | 34.9955° |
| perigee height: | 556 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 289.5808° |
| argument of perigee: | 248.9731° |
| revolutions per day: | 15.02546314 |
| mean anomaly at epoch: | 111.0474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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