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 28702U 26145.29938561 +.00000000 +00000-0 +00000-0 0 00003
2 28702 3.2423 79.2096 0003151 339.1381 265.2085 1.00271053 03
| Epoch (UTC): | 25 May 2026 07:11:06 |
| Eccentricity: | 0.0003151 |
| inclination: | 3.2423° |
| perigee height: | 35774 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 79.2096° |
| argument of perigee: | 339.1381° |
| revolutions per day: | 1.00271053 |
| mean anomaly at epoch: | 265.2085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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