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 28654U 26110.15753354 +.00000000 +00000-0 +34096-4 0 00007
2 28654 98.8115 190.6740 0013442 319.2191 40.7974 14.13718811 02
| Epoch (UTC): | 20 April 2026 03:46:50 |
| Eccentricity: | 0.0013442 |
| inclination: | 98.8115° |
| perigee height: | 837 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 190.6740° |
| argument of perigee: | 319.2191° |
| revolutions per day: | 14.13718811 |
| mean anomaly at epoch: | 40.7974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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