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 02802U 26088.08989802 +.00000000 +00000-0 +91647-4 0 00004
2 02802 74.0111 311.8596 0064885 313.8293 45.7511 14.45637631 04
| Epoch (UTC): | 29 March 2026 02:09:27 |
| Eccentricity: | 0.0064885 |
| inclination: | 74.0111° |
| perigee height: | 694 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 311.8596° |
| argument of perigee: | 313.8293° |
| revolutions per day: | 14.45637631 |
| mean anomaly at epoch: | 45.7511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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