▸Orbital parameters

Orbit class	SSO
Inclination	97.7556°
Eccentricity	0.0002986
Period	96.5 min
Apogee	595 km
Perigee	591 km
Mean motion	14.91654850 rev/day
RAAN	146.0262°
Arg of perigee	32.6629°
Mean anomaly	327.4774°
B*	1.9156e-4
Rev at epoch	1,470

▸Two-line element set (TLE)

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

1 68498U 26067CL 26188.19480624 .00001869 00000-0 19156-3 0 9994

2 68498 97.7556 146.0262 0002986 32.6629 327.4774 14.91654850 14709

▸ source OMM (JSON)

{
  "OBJECT_NAME": "IO-1",
  "OBJECT_ID": "2026-067CL",
  "EPOCH": "2026-07-07T04:40:31.259+00:00",
  "MEAN_MOTION": 14.9165485,
  "ECCENTRICITY": 0.0002986,
  "INCLINATION": 97.7556,
  "RA_OF_ASC_NODE": 146.0262,
  "ARG_OF_PERICENTER": 32.6629,
  "MEAN_ANOMALY": 327.4774,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68498,
  "REV_AT_EPOCH": 1470,
  "BSTAR": 0.00019156,
  "MEAN_MOTION_DOT": 0.00001869,
  "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	IO-1
Operator	Iota TechnologiesHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United Kingdom
Launch date	Mar 30, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	8HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/68498

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