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 26088.21730582 +.00000000 +00000-0 +59065-4 0 00009
2 28654 98.8130 169.0486 0014547 22.7420 337.4394 14.13714770 06
| Epoch (UTC): | 29 March 2026 05:12:55 |
| Eccentricity: | 0.0014547 |
| inclination: | 98.8130° |
| perigee height: | 836 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 169.0486° |
| argument of perigee: | 22.7420° |
| revolutions per day: | 14.13714770 |
| mean anomaly at epoch: | 337.4394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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