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 28649U 26067.60769111 +.00000000 +00000-0 +25887-3 0 00007
2 28649 97.5412 95.2030 0002376 70.8038 289.3438 14.90761114 03
| Epoch (UTC): | 08 March 2026 14:35:04 |
| Eccentricity: | 0.0002376 |
| inclination: | 97.5412° |
| perigee height: | 594 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 95.2030° |
| argument of perigee: | 70.8038° |
| revolutions per day: | 14.90761114 |
| mean anomaly at epoch: | 289.3438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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