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 26152.36703128 +.00000000 +00000-0 +27161-3 0 00001
2 28895 98.2967 307.6587 0012837 254.1655 105.8136 14.72584583 01
| Epoch (UTC): | 01 June 2026 08:48:31 |
| Eccentricity: | 0.0012837 |
| inclination: | 98.2967° |
| perigee height: | 644 km |
| apogee height: | 662 km |
| right ascension of ascending node: | 307.6587° |
| argument of perigee: | 254.1655° |
| revolutions per day: | 14.72584583 |
| mean anomaly at epoch: | 105.8136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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