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 28870U 26041.83056014 +.00000000 +00000-0 +12299-2 0 00003
2 28870 49.3475 196.7129 5376784 102.9097 319.7652 4.98629860 07
| Epoch (UTC): | 10 February 2026 19:56:00 |
| Eccentricity: | 0.5376784 |
| inclination: | 49.3475° |
| perigee height: | 313 km |
| apogee height: | 15876 km |
| right ascension of ascending node: | 196.7129° |
| argument of perigee: | 102.9097° |
| revolutions per day: | 4.98629860 |
| mean anomaly at epoch: | 319.7652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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