▸Orbital parameters

Orbit class	SSO
Inclination	98.6820°
Eccentricity	0.0009437
Period	100.6 min
Apogee	794 km
Perigee	780 km
Mean motion	14.31375033 rev/day
RAAN	255.0170°
Arg of perigee	33.2338°
Mean anomaly	326.9435°
B*	5.0471e-5
Rev at epoch	71,010

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 22826U 93061D 26187.69194507 .00000089 00000-0 50471-4 0 9992

2 22826 98.6820 255.0170 0009437 33.2338 326.9435 14.31375033710101

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ITAMSAT (IO-26)",
  "OBJECT_ID": "1993-061D",
  "EPOCH": "2026-07-06T16:36:24.054+00:00",
  "MEAN_MOTION": 14.31375033,
  "ECCENTRICITY": 0.0009437,
  "INCLINATION": 98.682,
  "RA_OF_ASC_NODE": 255.017,
  "ARG_OF_PERICENTER": 33.2338,
  "MEAN_ANOMALY": 326.9435,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 22826,
  "REV_AT_EPOCH": 71010,
  "BSTAR": 0.000050471,
  "MEAN_MOTION_DOT": 8.9e-7,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	ITAMSAT (IO-26)
Operator	Satellife IncHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree AMSATMEDIUMvia Wikidata
Country	ItalyMEDIUMvia Wikidata
Launch date	Sep 26, 1993HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	50HIGH

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/22826

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.