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 02872U 26145.43150565 +.00000000 +00000-0 +79713-4 0 00000
2 02872 69.9753 49.8292 0005801 167.4535 192.6718 13.99596685 04
| Epoch (UTC): | 25 May 2026 10:21:22 |
| Eccentricity: | 0.0005801 |
| inclination: | 69.9753° |
| perigee height: | 891 km |
| apogee height: | 899 km |
| right ascension of ascending node: | 49.8292° |
| argument of perigee: | 167.4535° |
| revolutions per day: | 13.99596685 |
| mean anomaly at epoch: | 192.6718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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