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 43677U 26153.60952528 +.00000000 +00000-0 +24556-3 0 00009
2 43677 98.0769 345.3575 0009984 162.4143 197.7428 15.02873320 00
| Epoch (UTC): | 02 June 2026 14:37:42 |
| Eccentricity: | 0.0009984 |
| inclination: | 98.0769° |
| perigee height: | 551 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 345.3575° |
| argument of perigee: | 162.4143° |
| revolutions per day: | 15.02873320 |
| mean anomaly at epoch: | 197.7428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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