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 02610U 26153.54113354 +.00000000 +00000-0 +16406-3 0 00005
2 02610 99.0953 327.9164 2271544 39.6531 335.0262 10.39896852 02
| Epoch (UTC): | 02 June 2026 12:59:13 |
| Eccentricity: | 0.2271544 |
| inclination: | 99.0953° |
| perigee height: | 474 km |
| apogee height: | 4502 km |
| right ascension of ascending node: | 327.9164° |
| argument of perigee: | 39.6531° |
| revolutions per day: | 10.39896852 |
| mean anomaly at epoch: | 335.0262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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