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 65988U 26145.36199294 +.00000000 +00000-0 +20851-3 0 00009
2 65988 81.3017 232.7063 0000392 236.7735 123.3384 13.84978653 06
| Epoch (UTC): | 25 May 2026 08:41:16 |
| Eccentricity: | 0.0000392 |
| inclination: | 81.3017° |
| perigee height: | 946 km |
| apogee height: | 947 km |
| right ascension of ascending node: | 232.7063° |
| argument of perigee: | 236.7735° |
| revolutions per day: | 13.84978653 |
| mean anomaly at epoch: | 123.3384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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