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 28661U 26069.45927464 +.00000000 +00000-0 +15580-2 0 00001
2 28661 49.3400 229.2376 5862139 105.4548 323.4141 4.29014903 07
| Epoch (UTC): | 10 March 2026 11:01:21 |
| Eccentricity: | 0.5862139 |
| inclination: | 49.3400° |
| perigee height: | 242 km |
| apogee height: | 18999 km |
| right ascension of ascending node: | 229.2376° |
| argument of perigee: | 105.4548° |
| revolutions per day: | 4.29014903 |
| mean anomaly at epoch: | 323.4141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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