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 28895U 26100.92775006 +.00000000 +00000-0 +24399-3 0 00000
2 28895 98.2897 255.1754 0015118 62.0932 298.1804 14.72457158 00
| Epoch (UTC): | 10 April 2026 22:15:57 |
| Eccentricity: | 0.0015118 |
| inclination: | 98.2897° |
| perigee height: | 643 km |
| apogee height: | 664 km |
| right ascension of ascending node: | 255.1754° |
| argument of perigee: | 62.0932° |
| revolutions per day: | 14.72457158 |
| mean anomaly at epoch: | 298.1804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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