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 40648U 26087.49299322 +.00000000 +00000-0 +44740-2 0 00009
2 40648 100.2069 276.6111 0037898 319.8425 39.9908 13.49523528 03
| Epoch (UTC): | 28 March 2026 11:49:54 |
| Eccentricity: | 0.0037898 |
| inclination: | 100.2069° |
| perigee height: | 1046 km |
| apogee height: | 1102 km |
| right ascension of ascending node: | 276.6111° |
| argument of perigee: | 319.8425° |
| revolutions per day: | 13.49523528 |
| mean anomaly at epoch: | 39.9908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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