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 66676U 26145.63559703 +.00000000 +00000-0 +23421-3 0 00005
2 66676 97.4181 219.3207 0007620 87.3448 272.8659 15.18762335 06
| Epoch (UTC): | 25 May 2026 15:15:15 |
| Eccentricity: | 0.0007620 |
| inclination: | 97.4181° |
| perigee height: | 504 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 219.3207° |
| argument of perigee: | 87.3448° |
| revolutions per day: | 15.18762335 |
| mean anomaly at epoch: | 272.8659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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