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 28898U 26065.81762255 +.00000000 +00000-0 +21133-3 0 00006
2 28898 98.3355 208.8680 0017412 302.6166 57.3355 14.64251798 06
| Epoch (UTC): | 06 March 2026 19:37:22 |
| Eccentricity: | 0.0017412 |
| inclination: | 98.3355° |
| perigee height: | 667 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 208.8680° |
| argument of perigee: | 302.6166° |
| revolutions per day: | 14.64251798 |
| mean anomaly at epoch: | 57.3355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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