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 26702U 26150.53587625 +.00000000 +00000-0 +13214-2 0 00008
2 26702 97.3881 190.4166 0005402 165.5322 194.6096 15.70091335 06
| Epoch (UTC): | 30 May 2026 12:51:39 |
| Eccentricity: | 0.0005402 |
| inclination: | 97.3881° |
| perigee height: | 355 km |
| apogee height: | 362 km |
| right ascension of ascending node: | 190.4166° |
| argument of perigee: | 165.5322° |
| revolutions per day: | 15.70091335 |
| mean anomaly at epoch: | 194.6096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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