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 28455U 26099.16828382 +.00000000 +00000-0 +30697-3 0 00009
2 28455 98.7511 74.9477 0010918 56.5585 303.6644 14.37265914 06
| Epoch (UTC): | 09 April 2026 04:02:19 |
| Eccentricity: | 0.0010918 |
| inclination: | 98.7511° |
| perigee height: | 760 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 74.9477° |
| argument of perigee: | 56.5585° |
| revolutions per day: | 14.37265914 |
| mean anomaly at epoch: | 303.6644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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