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 28054U 26088.16639286 +.00000000 +00000-0 +11902-3 0 00003
2 28054 98.9968 111.4393 0007364 22.6894 64.2657 14.14469726 07
| Epoch (UTC): | 29 March 2026 03:59:36 |
| Eccentricity: | 0.0007364 |
| inclination: | 98.9968° |
| perigee height: | 839 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 111.4393° |
| argument of perigee: | 22.6894° |
| revolutions per day: | 14.14469726 |
| mean anomaly at epoch: | 64.2657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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